{
  "schema": "FluentAGI-reproduction-v1",
  "run_id": "20261018-131135-2f3559",
  "request": "翼型绕流，也来一个，要求智能加密网格，自己定义，要求速度算快点，我现在在演示",
  "rounds": [
    {
      "round": "round-01",
      "prompt": "You are FluentAGI for Ansys Fluent. Write one short Chinese plan, then a single COMPLETE Python script in this exact Markdown layout:\n\n<fluent_code>\n\n```python\n# Use the existing connected PyFluent variable solver.\n# Continue with the complete executable script here.\n```\n\n</fluent_code>\n\nPut a newline before and after each tag and each fence. Put no prose, headings, units, or explanations inside the fenced Python block. Do not place ```python and Python statements on the same line. Keep the script under 280 lines. Use loops instead of repeating similar statements. Never truncate a string, parenthesis, or code fence; always close </fluent_code>.\nUse the existing solver session and compatible PyFluent APIs. A completed conversation turn does not close the session. For continuation requests reuse the loaded mesh and solution, inspect relevant current settings, and continue from actual flow time. Never launch, disconnect, remesh or initialize merely because a new desktop task directory was created. Do not launch or close Fluent. Do not use Abaqus APIs. Use solver.settings APIs and the provided fluentagi adapters. Direct solver.tui, execute_tui and Scheme remain rejected; the trusted v242 adapters may internally use fixed official TUI commands/journals. For mesh display use solver.settings.results.graphics.mesh and graphics.views APIs. Do not return JSON tool plans. Do not invent mesh files or API names. Only operate on the requested case and task directory. Preserve existing results. For a repair, inspect partially applied state and write a complete corrected script, not a patch or a repeated broken script.\nThe web AI cannot read or modify host application source. Do not claim to have searched the host disk or request uploading FluentAGI source to run simulations. Use the verified runtime adapters. Define task_directory as the absolute Task directory below before calling adapters. For VOF surface tension use fluentagi.configure_surface_tension(directory=task_directory,coefficient=0.072,phase_a=\"phase-1\",phase_b=\"phase-2\"); coefficient is N/m, replace the example with the requested value. This v242/v252 surface-tension adapter preserves other phase pairs, enables the surface-tension model and reads back every coefficient. inspect_surface_tension(directory=task_directory) returns actual state. Fluent 2025 R2 is accepted for this surface-tension adapter; do not ask to downgrade to 2024. Other Lee/DPM adapters retain their own version restrictions. Never claim v252 execution was validated before reading actual results. Do not ask the user to edit the plugin or click GUI dialogs for this supported operation.\nMixture and VOF both support Lee evaporation-condensation in official Fluent 2024 R2, but this runtime has NOT validated a Mixture configuration adapter. Do not silently substitute VOF for a Mixture tutorial or claim equivalent results. audit_multiphase_interfaces() is a read-only native settings probe, without TUI, Scheme or case writes. The VOF adapter uses narrowly scoped prompt profiles; unsupported dimension/phase combinations are rejected rather than guessed. For three-phase boiling setup in Fluent 2024 R2, use fluentagi.configure_three_phase_materials(directory=task_directory, materials=[\"air\", \"water-liquid\", \"water-vapor\"]) to create actual phase-1/2/3 domains and verify material assignments. For an existing three-phase model, fluentagi.assign_multiphase_materials(materials=[...], directory=task_directory) assigns materials without changing the phase count. Then call fluentagi.configure_evaporation_condensation(directory=task_directory, saturation_temperature=T_sat_K, evaporation_frequency=from_frequency_per_second, condensation_frequency=to_frequency_per_second, from_phase=\"phase-2\", to_phase=\"phase-3\"). Pass the user's specified temperature/frequencies; preserve their geometry, heating and calculation parameters. This verified v242 VOF Lee adapter enables energy, uses a fixed official TUI journal and verifies the phase pair, constant saturation temperature, both frequencies and Lee model by an independent case snapshot. It does not initialize or advance the simulation. Do not say this feature is unavailable because direct TUI is forbidden; use the adapter. fluentagi.inspect_phase_change(directory=task_directory) returns actual phases and mass transfer settings, refreshing a unique case snapshot. Do not replace existing unrelated mechanisms. This adapter supports one Lee mass transfer pair, not Eulerian wall boiling, semi-mechanistic wall boiling, pressure-dependent saturation tables or UDFs. Do not claim a complete validated boiling simulation from successful setup alone. initialize_air is a TWO-PHASE adapter; do not use it for three-phase cases. Use verified settings initialization and phase-aware patching only for requested new calculations.\nThe runtime provides fluentagi.assign_phase_materials(primary=\"air\", secondary=\"water-liquid\", directory=task_directory), fluentagi.inspect_phases(), and fluentagi.export_results(directory=task_directory, fields=[\"pressure\", \"velocity-magnitude\"]). For requested animation of an already initialized transient solution use fluentagi.record_animation(directory=task_directory, field=\"velocity-magnitude\", frames=10, steps_per_frame=1, max_iter_per_step=20); it advances the solution and creates PNG frames and GIF. Never initialize or advance an existing solution without the user requesting calculation. These are executable verified adapters, not prose instructions. Use the phase adapter when asked to assign materials; do not ask the user to click the phase dialog. Print returned results. For postprocessing use export_results and assess its errors; never claim missing images were saved. Only import math/json/itertools/functools/collections/dataclasses/typing; datetime/os/pathlib imports are unavailable. Check is_active() before querying model-dependent settings on an empty mesh.\nFor NEW planar geometry and meshing use mesh = fluentagi.build_planar(directory=task_directory, points=[[x,y],...], inlet_edges=[0], outlet_edges=[2], size=0.001). Coordinates and size are in METERS; polygon vertices ordered around its boundary; edge i joins point i to point (i+1)%N. This creates real STEP CAD and converts first-order triangular Gmsh cells into a genuine Fluent mesh with inlet/outlet/walls. Then solver.settings.file.read_mesh(file_name=mesh[\"mesh_file\"]), solver.settings.mesh.check(), configure physics, initialize, iterate, and export_results. Save current case/data before replacing loaded geometry. Do not reuse a model from previous successful construction during a repair; use its mesh_file from feedback. For curved planar CAD, use fluentagi.geometry_mesh(directory=task_directory,code=gmsh_script_string); the worker has gmsh,math,output_dir already, no imports; create OCC geometry and physical line groups named inlet,outlet,walls, export STEP, generate first-order triangular or quadrilateral mesh(2). Returned mesh_file is Fluent format; gmsh-native.msh is NOT Fluent format. 3D modeling and volume mesh conversion are now implemented. fluentagi.build_volume(directory=task_directory, shape=\"box\",length=0.1,width=0.02,height=0.02,size=0.005,mesh_type=\"tet\") creates tetrahedra; mesh_type=\"hex\" creates a structured all-hexahedron box. shape=\"cylinder\",radius=0.01 supports tetrahedra with axis along +X. Inlet is X=0 and outlet X=length. fluentagi.build_extruded(directory=task_directory,points=[[x,y],...],inlet_edges=[0],outlet_edges=[2],depth=0.01,size=0.002,mesh_type=\"tet\") extrudes a planar profile, naming lateral inlet/outlet faces; front/back faces are walls. mesh_type=\"hex-dominant\" uses recombined extruded mesh and MAY include prisms: assess returned cell_types, never call mixed cells pure hex. geometry_mesh supports arbitrary OCC volumes (boolean unions/cuts), physical SURFACE groups inlet/outlet/walls, and mesh.generate(3), first-order tet/hex/prism/pyramid. Imported STEP is not currently supported by the restricted worker. build_planar mesh_type=\"quad\" produces mapped pure quadrilaterals for valid four-sided rectangles; complex polygons can be quad/tri mixed. 2D uses triangles/quads, 3D uses tet/hex. The runtime starts or safely backs up its owned solver before switching dimension according to explicit user words. Do not request user-supplied 3D mesh for supported geometry. Save backups before replacing any loaded mesh. For 3D postprocessing create useful cut planes/isosurfaces using verified settings APIs; boundary-only contours are not an interior volume visualization. For an entire new analysis, carry out all stages rather than only inspection; collect real residual/convergence evidence and exports.\nFor water-air transient filling, call fluentagi.configure_water_air(directory=task_directory,velocity=0.05,time_step=0.001,gravity_y=-9.81,inlet=\"inlet\",outlet=\"outlet\"). This backs up and sets laminar VOF, materials, phase-aware inlet/outlet, gravity and timestep; does NOT initialize or erase existing solution. For requested NEW filling use fluentagi.initialize_air(directory=task_directory), which saves a backup, hybrid initializes and patches phase-2 volume fraction to zero across all fluid cell zones. Never initialize_air on existing results without an explicit restart request. Fluent v242 contour fields are phase-2-vof (water, only after confirming phase-2=water-liquid) and phase-1-vof (air); do not confuse them. Query real contour field.allowed_values for VOF fields. For 3D interior contours/animation use section=fluentagi.create_section(axis=\"z\",position=depth/2), then export_results(...,surfaces=[section[\"surface\"]]) or record_animation(...,surfaces=[section[\"surface\"]]). A plane section is not full volumetric rendering; report it accurately. Frames are 2..60. Each frame after the first advances steps_per_frame real time steps; final time is initial time+(frames-1)*steps_per_frame*time_step. Do not claim the pipe fills if the simulated duration is too short. Normalize typos like \"二维四面体\" by explaining 2D triangular equivalent; if depth/3D was explicitly requested, use volume tools.\nFor UNSTEADY dust motion use the separate transient DPM adapters, never track_particles (steady replay). build_dust_box(directory=task_directory) creates a 3D 40mm box with a top cylindrical nozzle (axis Y, inlet at top blowing DOWN with positive normal inlet speed) and an upper side pressure vent. Save existing case before reading its mesh_file. geometry parameters are SI and can be passed as named arguments. Choose suitable air physics; configure a real pressure outlet, do not create a sealed box with uncompensated inflow. configure_transient_dust(directory=task_directory,region_min=[.012,.003,.012],region_max=[.028,.004,.028],counts=[2,2,2],release_time=.02,release_duration=.0005,total_mass=1e-8,diameter=[1e-5,5e-5]*4,density=2500,initial_velocity=[0,0,0],gravity=[0,-9.81,0],time_step=.004,wall_behavior=\"trap\") enables actual unsteady air and one-way unsteady DPM. It creates one short native injection pulse for each seed; total_mass kg is distributed across weighted parcels. It accepts explicit points instead of a region. The entire release pulse must fit inside one physical dt. Does NOT initialize. For requested NEW cases only, initialize_transient_dust(directory=task_directory) refuses any existing valid solution. Then advance_transient_dust(directory=task_directory,until_time=.2,max_iter_per_step=200,residual_tolerance=.001) advances at most 60 actual steps per call, preferring an ABSOLUTE end time; read returned final_time and call again until target. Already reached until_time does not advance again. The small demonstration explicitly uses normalized residual tolerance .001; honor stricter user requirements and never silently relax them. The default adapter tolerance is 1e-5, which the coarse benchmark did NOT meet on its initial step. Failed per-step convergence/air mass balance/particle accounting stops with needs_review and a checkpoint; never claim success. read_transient_dust(directory=task_directory) reads actual current native particle positions, fates, masses and physical time without advancement. resume_transient_dust(directory=task_directory,checkpoint=\"latest-checkpoint.json\") backs up current case, validates hashes, restores native Case/Data including particles, and verifies actual state; never initializes. read_transient_dust_results(directory=task_directory) reads saved files offline. On continuation reuse the ORIGINAL batch directory from execution feedback for read/resume/advance; do not create another configuration merely because the desktop has a new task directory. Native output remains with the original case, while preview PNG/GIF/CSV are mirrored into the current desktop task for real-time display. Every frame is a snapshot of native transient particles, not a steady trajectory interpolation. Report deposited/trapped, escaped, in-domain, incomplete, aborted and not-yet-released parcels and actual mass budget. Caption all runs \"预先释放悬浮颗粒，非积尘再悬浮\". Particle seeds/markers represent weighted parcels, not physical particle counts or true point size. Laminar transport shows resolved advection/settling; do not claim stochastic turbulent diffusion is modeled. No verified deposited-dust detachment/adhesion/UDF resuspension adapter exists. Never add an upward initial velocity and call it resuspension. Preserve steady DPM as a distinct path.\nFor EXPLICITLY STEADY dilute solid dust ONLY use the verified v242 one-way STEADY DPM adapters, not VOF. First inspect_dpm(). On a single-phase carrier first create_dust_injection with the required density (default 2500 kg/m3) to activate actual inert materials, THEN configure_dpm(directory=task_directory,density=2500,material=\"agi-dust\",max_steps=10000) verifies the inert material density and sets tracking limit; never use solid CAD material. The v242 inert material container has an unreliable active flag/get_state; adapters enumerate named material children and read those real states instead. Never query the entire inert material container. create_dust_injection(directory=task_directory,name=\"dust\",start=[0.00001,0.003,0.01],end=[0.00001,0.017,0.01],streams=12,diameter=0.00005,mass_flow=0.0000001,velocity=[0.5,0,0],material=\"agi-dust\") creates a real group injection. Replace positions with points just INSIDE the actual inlet; SI meters, diameter meters, mass_flow TOTAL kg/s (adapter divides over streams). streams=1 creates a single injection; group uses a release line between start/end. Do not use surface injection; its v242 settings readback failed validation. set_particle_boundaries(directory=task_directory,boundaries={\"inlet\":\"escape\",\"outlet\":\"escape\",\"walls\":\"trap\"}) also supports reflect with existing restitution settings; always inspect readback. Never silently change an existing multiphase or coupled DPM model. For a requested NEW analysis, configure and solve the AIR carrier first (laminar only for suitable low Reynolds), then track_particles(directory=task_directory,injections=[\"dust\"],frames=30). This tracks native DPM trajectories, exports tracks.csv/json, native summary text, statistics and PNG/GIF. It does NOT initialize or advance the carrier. Animation is a residence-time replay of native STEADY particle tracks with simultaneous release, not a transient fluid/DPM calculation. Never use air pathlines or a continuous-phase contour as dust motion. Returned counts refer to particle streams, not physical dust counts; rates use reported mass flow. Report incomplete/aborted streams, mass/count balance and carrier convergence separately. A successful track/image is not validated collection efficiency; require mesh/physics validation for engineering conclusions. Preserve results; use a new injection name if its parameters change.\nEnd with <final_answer>Chinese explanation of the intended changes, without claiming execution success</final_answer>.\nIf essential input or an incompatible session prevents a valid script, return only <question>the specific missing input in Chinese</question>.\nAfter the desktop returns execution results, either provide a corrected script or return only <final_answer>a Chinese assessment supported by those results</final_answer>. Do not execute the same successful script again. Successful execution alone does not prove convergence.\n\nPrevious conversation and execution context (reference only; do not repeat successful scripts):\n[{\"user\": \"创建长 0.2 m、高 0.02 m 的二维流道，通过 build_planar 生成 STEP 和尺寸 0.001 m 的三角形 Fluent 网格。空气层流，入口速度 0.1 m/s，出口表压 0 Pa，上下壁面无滑移。分批迭代检查收敛，保存 case/data。\"}, {\"assistant\": \"找不到输入框；请完成登录/真人验证，或在设置中更新网页选择器。\", \"run_directory\": \"C:\\\\Users\\\\13977\\\\AppData\\\\Local\\\\FluentAGI\\\\data\\\\runs\\\\20261018-130631-f68176\"}, {\"user\": \"继续\"}, {\"tool\": \"run_code\", \"result\": \"{\\\"status\\\": \\\"ok\\\", \\\"stdout\\\": \\\"\\\\nOpening input/output transcript to file \\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-130707-27e2af\\\\\\\\channel_velocity_repair.trn\\\\\\\".\\\\n\\\\n Domain Extents:\\\\n   x-coordinate: min (m) = 0.000000e+00, max (m) = 2.000000e-01\\\\n   y-coordinate: min (m) = 0.000000e+00, max (m) = 2.000000e-02\\\\n Volume statistics:\\\\n   minimum volume (m3): 2.695799e-07\\\\n   maximum volume (m3): 5.611842e-07\\\\n     total volume (m3): 4.000000e-03\\\\n Face area statistics:\\\\n\\n…中间日志已省略，完整日志保存在任务目录…\\n       9258 cells,     1 zone  ...\\\\n       14107 faces,     4 zones ...\\\\n        4850 nodes,     1 zone  ...\\\\n  Done.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-130707-27e2af\\\\\\\\channel_velocity_repair_final.dat.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\n  Writing results.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-130707-27e2af\\\\\\\\post-130923-6f2c\\\\\\\\result.cas.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\nGrouping cells for Laplace smoothing ...\\\\n        9258 cells,     1 zone  ...\\\\n       14107 faces,     4 zones ...\\\\n        4850 nodes,     1 zone  ...\\\\n  Done.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-130707-27e2af\\\\\\\\post-130923-6f2c\\\\\\\\result.dat.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\n  Writing results.\\\\nDone.\\\\nCreating zone surface for fluid zone\\\\nEXPORT_RESULTS {'status': 'ok', 'directory': 'C:\\\\\\\\\\\\\\\\Users\\\\\\\\\\\\\\\\13977\\\\\\\\\\\\\\\\AppData\\\\\\\\\\\\\\\\Local\\\\\\\\\\\\\\\\FluentAGI\\\\\\\\\\\\\\\\data\\\\\\\\\\\\\\\\runs\\\\\\\\\\\\\\\\20261018-130707-27e2af\\\\\\\\\\\\\\\\post-130923-6f2c', 'created': '2026-10-18T13:09:23.686944', 'files': ['mesh.png', 'pressure.png', 'residual.csv', 'result.cas.h5', 'result.dat.h5', 'velocity-magnitude.png'], 'errors': [], 'convergence_verified': False}\\\\n实际残差和收敛提示记录在 channel_velocity_repair.trn；请结合各批日志判断收敛，导出文件以适配器实际返回结果为准。\\\\n\\\\nTranscript closed.\\\\n\\\", \\\"stderr\\\": \\\"\\\", \\\"return_value\\\": null, \\\"message\\\": null, \\\"error_code\\\": null, \\\"warnings\\\": []}\"}, {\"assistant\": \"本次已完成计算与保存，无需重复运行。\\n\\n网格：9258 个三角形单元，4850 个节点。\\n最终第 36 次迭代，Fluent 明确提示“solution is converged”，达到当前设置的残差判据。\\n最终残差：连续性 3.4656×10⁻⁴，x 速度 3.9597×10⁻⁶，y 速度 1.5044×10⁻⁷。\\n已保存最终 case/data：channel_velocity_repair_final.cas.h5、channel_velocity_repair_final.dat.h5。\\n后处理目录 post-130923-6f2c 已导出网格图、压力图、速度图和 residual.csv，返回错误列表为空。\\n\\n上述证据说明当前残差判据已满足；质量守恒误差和网格无关性尚未验证。\", \"run_directory\": \"C:\\\\Users\\\\13977\\\\AppData\\\\Local\\\\FluentAGI\\\\data\\\\runs\\\\20261018-130707-27e2af\"}, {\"user\": \"翼型绕流，也来一个，要求智能加密网格，自己定义，要求速度算快点，我现在在演示\"}]\nRuntime capabilities:\n{\"protocol\": \"FluentAGI-capabilities-v1\", \"session\": {\"connected\": true, \"mode\": \"launch\"}, \"geometry\": {\"worker\": \"gmsh isolated process\", \"imports\": [], \"builtins\": [\"range\", \"len\", \"int\", \"float\", \"str\", \"list\", \"tuple\", \"enumerate\", \"zip\", \"min\", \"max\", \"abs\", \"round\", \"RuntimeError\", \"ValueError\", \"print\", \"set\", \"sum\", \"sorted\", \"bool\", \"all\", \"any\"], \"physical_groups\": [\"inlet\", \"outlet\", \"walls\"], \"cell_types\": [\"triangle\", \"quadrilateral\", \"tetrahedron\", \"hexahedron\", \"prism\", \"pyramid\"]}, \"script\": {\"imports\": [\"math\", \"json\", \"itertools\", \"functools\", \"collections\", \"dataclasses\", \"typing\"], \"adapters\": [\"build_dust_box\", \"configure_transient_dust\", \"initialize_transient_dust\", \"read_transient_dust\", \"advance_transient_dust\", \"resume_transient_dust\", \"read_transient_dust_results\", \"inspect_dpm\", \"configure_dpm\", \"create_dust_injection\", \"set_particle_boundaries\", \"track_particles\", \"build_planar\", \"build_volume\", \"build_extruded\", \"geometry_mesh\", \"configure_water_air\", \"initialize_air\", \"record_animation\", \"export_results\", \"assign_phase_materials\", \"assign_multiphase_materials\", \"configure_three_phase_materials\", \"audit_multiphase_interfaces\", \"configure_evaporation_condensation\", \"inspect_phase_change\", \"configure_surface_tension\", \"inspect_surface_tension\"]}, \"generated_at\": 1792300295.565992, \"phase_change\": {\"version\": \"v242\", \"model\": \"Lee\", \"adapter_multiphase_models\": [\"vof\"], \"mixture_officially_available\": true, \"mixture_adapter_validated\": false, \"two_phase_2d_correction_runtime_validation\": \"pending\", \"automatic_model_switch\": false, \"phases\": [2, 3], \"saturation\": \"constant K\", \"frequencies\": \"positive finite 1/s\", \"mass_transfer_pairs\": 1, \"internal_official_tui\": true, \"generated_direct_tui\": false, \"readback\": \"unique case snapshot\", \"initializes\": false}, \"surface_tension\": {\"version\": \"v242/v252\", \"runtime_validation\": {\"v242\": \"previous native validation\", \"v252\": \"official command and generated SDK checked; customer runtime readback required\"}, \"model\": \"VOF\", \"coefficient\": \"nonnegative finite N/m\", \"preserves_other_pairs\": true, \"readback\": \"unique case snapshot\", \"initializes\": false}, \"transient_dpm\": {\"version\": \"v242\", \"model\": \"unsteady single-phase carrier + transient one-way inert DPM\", \"release\": \"one short native pulse per explicit point / region grid, max 64 weighted parcels\", \"chunk_steps\": 60, \"positions\": \"native current positions at actual physical time; never steady replay\", \"checkpoint\": \"unique Case/Data plus SHA256 and particle-state readback\", \"acceptance\": \"each-step residuals, native air mass flux, particle mass/count fate closure\", \"default_residual_tolerance\": 1e-05, \"benchmark_residual_tolerance\": 0.001, \"strict_1e_5_initial_step_validated\": false, \"resuspension_validated\": false, \"stochastic_turbulent_dispersion_validated\": false}, \"dpm\": {\"version\": \"v242\", \"carrier\": \"single phase, one-way, steady inert dust\", \"injection_types\": [\"single\", \"group\"], \"surface_injection_validated\": false, \"boundary_types\": [\"reflect\", \"trap\", \"escape\"], \"trajectory_source\": \"native GetParticleTracksField RPC\", \"animation\": \"steady DPM trajectory residence-time replay, no carrier advance\", \"transient_dpm_validated\": false, \"two_way_validated\": false, \"readback\": true, \"active\": true}, \"fluent_version\": \"Ansys Fluent 2024 R2\", \"model_active\": true}\nCurrent session:\n{\"connected\": true, \"dimension\": 2, \"mode\": \"solver\", \"owned\": true, \"continuation\": true}\nTask directory:\nC:\\Users\\13977\\AppData\\Local\\FluentAGI\\data\\runs\\20261018-131135-2f3559\nCurrent request:\n翼型绕流，也来一个，要求智能加密网格，自己定义，要求速度算快点，我现在在演示",
      "reply": "ChatGPT 说：\n\n采用二维 NACA0012 翼型、零攻角低速空气层流演示；自动加密翼面、前缘和尾迹，远场用粗网格，先备份当前流道，再分批求解并导出云图。\n\n<fluent_code>\n```python\n# Use the existing connected PyFluent variable solver.\ntask_directory = r\"C:\\Users\\13977\\AppData\\Local\\FluentAGI\\data\\runs\\20261018-131135-2f3559\"\nsettings = solver.settings\ntranscript_started = False\n\ngmsh_code = \"\"\"\ngmsh.model.add(\"naca0012_fast_demo\")\nocc = gmsh.model.occ\nchord = 0.1\nn = 36\nupper = []\nlower = []\nfor i in range(n + 1):\n    x = 0.5 * (1.0 - math.cos(math.pi * i / n))\n    yt = 5.0 * 0.12 * (\n        0.2969 * math.sqrt(x)\n        - 0.1260 * x\n        - 0.3516 * x * x\n        + 0.2843 * x * x * x\n        - 0.1036 * x * x * x * x\n    )\n    if i == 0 or i == n:\n        p = occ.addPoint(chord * x, 0.0, 0.0)\n        upper.append(p)\n        lower.append(p)\n    else:\n        upper.append(occ.addPoint(chord * x, chord * yt, 0.0))\n        lower.append(occ.addPoint(chord * x, -chord * yt, 0.0))\n\ncu = occ.addSpline(upper)\ncl = occ.addSpline(list(reversed(lower)))\nfoil_loop = occ.addCurveLoop([cu, cl])\np0 = occ.addPoint(-0.3, -0.3, 0)\np1 = occ.addPoint(0.7, -0.3, 0)\np2 = occ.addPoint(0.7, 0.3, 0)\np3 = occ.addPoint(-0.3, 0.3, 0)\nbottom = occ.addLine(p0, p1)\nright = occ.addLine(p1, p2)\ntop = occ.addLine(p2, p3)\nleft = occ.addLine(p3, p0)\nouter_loop = occ.addCurveLoop([bottom, right, top, left])\nfluid = occ.addPlaneSurface([outer_loop, foil_loop])\nocc.synchronize()\n\nfor name, curves in [\n    (\"inlet\", [left]),\n    (\"outlet\", [right]),\n    (\"walls\", [bottom, top, cu, cl]),\n]:\n    tag = gmsh.model.addPhysicalGroup(1, curves)\n    gmsh.model.setPhysicalName(1, tag, name)\ntag = gmsh.model.addPhysicalGroup(2, [fluid])\ngmsh.model.setPhysicalName(2, tag, \"fluid\")\n\ndistance = gmsh.model.mesh.field.add(\"Distance\")\ngmsh.model.mesh.field.setNumbers(distance, \"CurvesList\", [cu, cl])\ngmsh.model.mesh.field.setNumber(distance, \"Sampling\", 160)\nnear = gmsh.model.mesh.field.add(\"Threshold\")\ngmsh.model.mesh.field.setNumber(near, \"InField\", distance)\ngmsh.model.mesh.field.setNumber(near, \"SizeMin\", 0.0008)\ngmsh.model.mesh.field.setNumber(near, \"SizeMax\", 0.025)\ngmsh.model.mesh.field.setNumber(near, \"DistMin\", 0.003)\ngmsh.model.mesh.field.setNumber(near, \"DistMax\", 0.08)\n\nwake = gmsh.model.mesh.field.add(\"Box\")\nfor key, value in [\n    (\"VIn\", 0.004), (\"VOut\", 0.025),\n    (\"XMin\", 0.085), (\"XMax\", 0.4),\n    (\"YMin\", -0.025), (\"YMax\", 0.025),\n    (\"ZMin\", -0.001), (\"ZMax\", 0.001),\n    (\"Thickness\", 0.025),\n]:\n    gmsh.model.mesh.field.setNumber(wake, key, value)\ncombined = gmsh.model.mesh.field.add(\"Min\")\ngmsh.model.mesh.field.setNumbers(combined, \"FieldsList\", [near, wake])\ngmsh.model.mesh.field.setAsBackgroundMesh(combined)\ngmsh.option.setNumber(\"Mesh.MeshSizeFromPoints\", 0)\ngmsh.option.setNumber(\"Mesh.MeshSizeFromCurvature\", 0)\ngmsh.option.setNumber(\"Mesh.MeshSizeExtendFromBoundary\", 0)\ngmsh.option.setNumber(\"Mesh.MeshSizeMin\", 0.0006)\ngmsh.option.setNumber(\"Mesh.MeshSizeMax\", 0.025)\ngmsh.option.setNumber(\"Mesh.ElementOrder\", 1)\ngmsh.option.setNumber(\"Mesh.Algorithm\", 6)\ngmsh.write(output_dir + \"/naca0012.step\")\ngmsh.model.mesh.generate(2)\ngmsh.model.mesh.optimize(\"Relocate2D\")\n\"\"\"\n\ntry:\n    settings.file.start_transcript(\n        file_name=task_directory + r\"\\airfoil_demo.trn\"\n    )\n    transcript_started = True\n\n    if settings.setup.models.is_active():\n        settings.file.write_case_data(\n            file_name=task_directory + r\"\\previous_channel_backup.cas.h5\"\n        )\n\n    mesh = fluentagi.geometry_mesh(\n        directory=task_directory,\n        code=gmsh_code,\n    )\n    print(\"AIRFOIL_MESH\", mesh)\n    settings.file.read_mesh(file_name=mesh[\"mesh_file\"])\n    settings.mesh.check()\n\n    if not settings.setup.models.is_active():\n        raise RuntimeError(\"翼型网格读取后模型未激活。\")\n\n    settings.setup.general.solver.type = \"pressure-based\"\n    settings.setup.general.solver.time = \"steady\"\n    settings.setup.models.viscous.model = \"laminar\"\n    settings.setup.models.energy.enabled = False\n    settings.setup.general.operating_conditions.gravity.enable = False\n\n    air = settings.setup.materials.fluid[\"air\"]\n    air.density.set_state({\"option\": \"constant\", \"value\": 1.225})\n    air.viscosity.set_state({\"option\": \"constant\", \"value\": 1.7894e-5})\n    print(\"AIR\", air.get_state())\n    print(\"DEMO_PARAMETERS\", {\n        \"airfoil\": \"NACA0012\",\n        \"chord_m\": 0.1,\n        \"velocity_m_s\": 0.1,\n        \"angle_deg\": 0.0,\n        \"Re_chord\": 1.225 * 0.1 * 0.1 / 1.7894e-5,\n        \"model\": \"steady laminar\",\n        \"refinement\": \"prescribed distance and wake fields\",\n    })\n\n    zones = settings.setup.cell_zone_conditions.fluid\n    for name in zones.get_object_names():\n        zones[name].general.material = \"air\"\n\n    boundaries = settings.setup.boundary_conditions\n    inlet = boundaries.velocity_inlet[\"inlet\"]\n    inlet.momentum.velocity_specification_method = \"Magnitude, Normal to Boundary\"\n    inlet.momentum.velocity.set_state({\"option\": \"value\", \"value\": 0.1})\n    outlet = boundaries.pressure_outlet[\"outlet\"]\n    outlet.momentum.gauge_pressure.set_state(\n        {\"option\": \"value\", \"value\": 0.0}\n    )\n    for name in boundaries.wall.get_object_names():\n        wall = boundaries.wall[name]\n        wall.momentum.wall_motion = \"Stationary Wall\"\n        wall.momentum.shear_condition = \"No Slip\"\n\n    print(\"INLET\", inlet.get_state())\n    print(\"OUTLET\", outlet.get_state())\n    print(\"WALLS\", boundaries.wall.get_state())\n    print(\"RESIDUAL_SETTINGS\", settings.solution.monitor.residual.get_state())\n\n    settings.file.write_case(\n        file_name=task_directory + r\"\\airfoil_configured.cas.h5\"\n    )\n    settings.solution.initialization.hybrid_initialize()\n\n    for batch in range(1, 4):\n        print(\"BATCH_BEGIN\", batch, \"MAX_ITERATIONS\", 100)\n        settings.solution.run_calculation.iterate(iter_count=100)\n        print(\"BATCH_END\", batch)\n        settings.file.write_case_data(\n            file_name=task_directory\n            + r\"\\airfoil_batch_\"\n            + str(batch)\n            + \".cas.h5\"\n        )\n\n    settings.file.write_case_data(\n        file_name=task_directory + r\"\\airfoil_final.cas.h5\"\n    )\n    result = fluentagi.export_results(\n        directory=task_directory,\n        fields=[\"pressure\", \"velocity-magnitude\"],\n    )\n    print(\"EXPORT_RESULTS\", result)\n    print(\n        \"本案例为低雷诺数零攻角风洞演示，采用预设空间局部加密，\"\n        \"不是基于求解误差的自适应网格。\"\n        \"实际收敛需核对 airfoil_demo.trn 和导出的 residual.csv；\"\n        \"若未达到判据，保留当前解继续迭代，不重新初始化。\"\n    )\n\nfinally:\n    if transcript_started:\n        settings.file.stop_transcript()\n```\n</fluent_code>\n\n<final_answer>拟建立弦长 0.1 m、入口速度 0.1 m/s 的 NACA0012 演示，翼面附近网格约 0.8 mm、尾迹约 4 mm、远场约 25 mm，以控制计算量。原流道先备份，计算后保存新 case/data 并导出网格、压力和速度图；运行时间及收敛情况以实际反馈为准。</final_answer>",
      "executed_script": "# Use the existing connected PyFluent variable solver.\ntask_directory = r\"C:\\Users\\13977\\AppData\\Local\\FluentAGI\\data\\runs\\20261018-131135-2f3559\"\nsettings = solver.settings\ntranscript_started = False\n\ngmsh_code = \"\"\"\ngmsh.model.add(\"naca0012_fast_demo\")\nocc = gmsh.model.occ\nchord = 0.1\nn = 36\nupper = []\nlower = []\nfor i in range(n + 1):\n    x = 0.5 * (1.0 - math.cos(math.pi * i / n))\n    yt = 5.0 * 0.12 * (\n        0.2969 * math.sqrt(x)\n        - 0.1260 * x\n        - 0.3516 * x * x\n        + 0.2843 * x * x * x\n        - 0.1036 * x * x * x * x\n    )\n    if i == 0 or i == n:\n        p = occ.addPoint(chord * x, 0.0, 0.0)\n        upper.append(p)\n        lower.append(p)\n    else:\n        upper.append(occ.addPoint(chord * x, chord * yt, 0.0))\n        lower.append(occ.addPoint(chord * x, -chord * yt, 0.0))\n\ncu = occ.addSpline(upper)\ncl = occ.addSpline(list(reversed(lower)))\nfoil_loop = occ.addCurveLoop([cu, cl])\np0 = occ.addPoint(-0.3, -0.3, 0)\np1 = occ.addPoint(0.7, -0.3, 0)\np2 = occ.addPoint(0.7, 0.3, 0)\np3 = occ.addPoint(-0.3, 0.3, 0)\nbottom = occ.addLine(p0, p1)\nright = occ.addLine(p1, p2)\ntop = occ.addLine(p2, p3)\nleft = occ.addLine(p3, p0)\nouter_loop = occ.addCurveLoop([bottom, right, top, left])\nfluid = occ.addPlaneSurface([outer_loop, foil_loop])\nocc.synchronize()\n\nfor name, curves in [\n    (\"inlet\", [left]),\n    (\"outlet\", [right]),\n    (\"walls\", [bottom, top, cu, cl]),\n]:\n    tag = gmsh.model.addPhysicalGroup(1, curves)\n    gmsh.model.setPhysicalName(1, tag, name)\ntag = gmsh.model.addPhysicalGroup(2, [fluid])\ngmsh.model.setPhysicalName(2, tag, \"fluid\")\n\ndistance = gmsh.model.mesh.field.add(\"Distance\")\ngmsh.model.mesh.field.setNumbers(distance, \"CurvesList\", [cu, cl])\ngmsh.model.mesh.field.setNumber(distance, \"Sampling\", 160)\nnear = gmsh.model.mesh.field.add(\"Threshold\")\ngmsh.model.mesh.field.setNumber(near, \"InField\", distance)\ngmsh.model.mesh.field.setNumber(near, \"SizeMin\", 0.0008)\ngmsh.model.mesh.field.setNumber(near, \"SizeMax\", 0.025)\ngmsh.model.mesh.field.setNumber(near, \"DistMin\", 0.003)\ngmsh.model.mesh.field.setNumber(near, \"DistMax\", 0.08)\n\nwake = gmsh.model.mesh.field.add(\"Box\")\nfor key, value in [\n    (\"VIn\", 0.004), (\"VOut\", 0.025),\n    (\"XMin\", 0.085), (\"XMax\", 0.4),\n    (\"YMin\", -0.025), (\"YMax\", 0.025),\n    (\"ZMin\", -0.001), (\"ZMax\", 0.001),\n    (\"Thickness\", 0.025),\n]:\n    gmsh.model.mesh.field.setNumber(wake, key, value)\ncombined = gmsh.model.mesh.field.add(\"Min\")\ngmsh.model.mesh.field.setNumbers(combined, \"FieldsList\", [near, wake])\ngmsh.model.mesh.field.setAsBackgroundMesh(combined)\ngmsh.option.setNumber(\"Mesh.MeshSizeFromPoints\", 0)\ngmsh.option.setNumber(\"Mesh.MeshSizeFromCurvature\", 0)\ngmsh.option.setNumber(\"Mesh.MeshSizeExtendFromBoundary\", 0)\ngmsh.option.setNumber(\"Mesh.MeshSizeMin\", 0.0006)\ngmsh.option.setNumber(\"Mesh.MeshSizeMax\", 0.025)\ngmsh.option.setNumber(\"Mesh.ElementOrder\", 1)\ngmsh.option.setNumber(\"Mesh.Algorithm\", 6)\ngmsh.write(output_dir + \"/naca0012.step\")\ngmsh.model.mesh.generate(2)\ngmsh.model.mesh.optimize(\"Relocate2D\")\n\"\"\"\n\ntry:\n    settings.file.start_transcript(\n        file_name=task_directory + r\"\\airfoil_demo.trn\"\n    )\n    transcript_started = True\n\n    if settings.setup.models.is_active():\n        settings.file.write_case_data(\n            file_name=task_directory + r\"\\previous_channel_backup.cas.h5\"\n        )\n\n    mesh = fluentagi.geometry_mesh(\n        directory=task_directory,\n        code=gmsh_code,\n    )\n    print(\"AIRFOIL_MESH\", mesh)\n    settings.file.read_mesh(file_name=mesh[\"mesh_file\"])\n    settings.mesh.check()\n\n    if not settings.setup.models.is_active():\n        raise RuntimeError(\"翼型网格读取后模型未激活。\")\n\n    settings.setup.general.solver.type = \"pressure-based\"\n    settings.setup.general.solver.time = \"steady\"\n    settings.setup.models.viscous.model = \"laminar\"\n    settings.setup.models.energy.enabled = False\n    settings.setup.general.operating_conditions.gravity.enable = False\n\n    air = settings.setup.materials.fluid[\"air\"]\n    air.density.set_state({\"option\": \"constant\", \"value\": 1.225})\n    air.viscosity.set_state({\"option\": \"constant\", \"value\": 1.7894e-5})\n    print(\"AIR\", air.get_state())\n    print(\"DEMO_PARAMETERS\", {\n        \"airfoil\": \"NACA0012\",\n        \"chord_m\": 0.1,\n        \"velocity_m_s\": 0.1,\n        \"angle_deg\": 0.0,\n        \"Re_chord\": 1.225 * 0.1 * 0.1 / 1.7894e-5,\n        \"model\": \"steady laminar\",\n        \"refinement\": \"prescribed distance and wake fields\",\n    })\n\n    zones = settings.setup.cell_zone_conditions.fluid\n    for name in zones.get_object_names():\n        zones[name].general.material = \"air\"\n\n    boundaries = settings.setup.boundary_conditions\n    inlet = boundaries.velocity_inlet[\"inlet\"]\n    inlet.momentum.velocity_specification_method = \"Magnitude, Normal to Boundary\"\n    inlet.momentum.velocity.set_state({\"option\": \"value\", \"value\": 0.1})\n    outlet = boundaries.pressure_outlet[\"outlet\"]\n    outlet.momentum.gauge_pressure.set_state(\n        {\"option\": \"value\", \"value\": 0.0}\n    )\n    for name in boundaries.wall.get_object_names():\n        wall = boundaries.wall[name]\n        wall.momentum.wall_motion = \"Stationary Wall\"\n        wall.momentum.shear_condition = \"No Slip\"\n\n    print(\"INLET\", inlet.get_state())\n    print(\"OUTLET\", outlet.get_state())\n    print(\"WALLS\", boundaries.wall.get_state())\n    print(\"RESIDUAL_SETTINGS\", settings.solution.monitor.residual.get_state())\n\n    settings.file.write_case(\n        file_name=task_directory + r\"\\airfoil_configured.cas.h5\"\n    )\n    settings.solution.initialization.hybrid_initialize()\n\n    for batch in range(1, 4):\n        print(\"BATCH_BEGIN\", batch, \"MAX_ITERATIONS\", 100)\n        settings.solution.run_calculation.iterate(iter_count=100)\n        print(\"BATCH_END\", batch)\n        settings.file.write_case_data(\n            file_name=task_directory\n            + r\"\\airfoil_batch_\"\n            + str(batch)\n            + \".cas.h5\"\n        )\n\n    settings.file.write_case_data(\n        file_name=task_directory + r\"\\airfoil_final.cas.h5\"\n    )\n    result = fluentagi.export_results(\n        directory=task_directory,\n        fields=[\"pressure\", \"velocity-magnitude\"],\n    )\n    print(\"EXPORT_RESULTS\", result)\n    print(\n        \"本案例为低雷诺数零攻角风洞演示，采用预设空间局部加密，\"\n        \"不是基于求解误差的自适应网格。\"\n        \"实际收敛需核对 airfoil_demo.trn 和导出的 residual.csv；\"\n        \"若未达到判据，保留当前解继续迭代，不重新初始化。\"\n    )\n\nfinally:\n    if transcript_started:\n        settings.file.stop_transcript()"
    },
    {
      "round": "round-02",
      "prompt": "You are FluentAGI for Ansys Fluent. Write one short Chinese plan, then a single COMPLETE Python script in this exact Markdown layout:\n\n<fluent_code>\n\n```python\n# Use the existing connected PyFluent variable solver.\n# Continue with the complete executable script here.\n```\n\n</fluent_code>\n\nPut a newline before and after each tag and each fence. Put no prose, headings, units, or explanations inside the fenced Python block. Do not place ```python and Python statements on the same line. Keep the script under 280 lines. Use loops instead of repeating similar statements. Never truncate a string, parenthesis, or code fence; always close </fluent_code>.\nUse the existing solver session and compatible PyFluent APIs. A completed conversation turn does not close the session. For continuation requests reuse the loaded mesh and solution, inspect relevant current settings, and continue from actual flow time. Never launch, disconnect, remesh or initialize merely because a new desktop task directory was created. Do not launch or close Fluent. Do not use Abaqus APIs. Use solver.settings APIs and the provided fluentagi adapters. Direct solver.tui, execute_tui and Scheme remain rejected; the trusted v242 adapters may internally use fixed official TUI commands/journals. For mesh display use solver.settings.results.graphics.mesh and graphics.views APIs. Do not return JSON tool plans. Do not invent mesh files or API names. Only operate on the requested case and task directory. Preserve existing results. For a repair, inspect partially applied state and write a complete corrected script, not a patch or a repeated broken script.\nThe web AI cannot read or modify host application source. Do not claim to have searched the host disk or request uploading FluentAGI source to run simulations. Use the verified runtime adapters. Define task_directory as the absolute Task directory below before calling adapters. For VOF surface tension use fluentagi.configure_surface_tension(directory=task_directory,coefficient=0.072,phase_a=\"phase-1\",phase_b=\"phase-2\"); coefficient is N/m, replace the example with the requested value. This v242/v252 surface-tension adapter preserves other phase pairs, enables the surface-tension model and reads back every coefficient. inspect_surface_tension(directory=task_directory) returns actual state. Fluent 2025 R2 is accepted for this surface-tension adapter; do not ask to downgrade to 2024. Other Lee/DPM adapters retain their own version restrictions. Never claim v252 execution was validated before reading actual results. Do not ask the user to edit the plugin or click GUI dialogs for this supported operation.\nMixture and VOF both support Lee evaporation-condensation in official Fluent 2024 R2, but this runtime has NOT validated a Mixture configuration adapter. Do not silently substitute VOF for a Mixture tutorial or claim equivalent results. audit_multiphase_interfaces() is a read-only native settings probe, without TUI, Scheme or case writes. The VOF adapter uses narrowly scoped prompt profiles; unsupported dimension/phase combinations are rejected rather than guessed. For three-phase boiling setup in Fluent 2024 R2, use fluentagi.configure_three_phase_materials(directory=task_directory, materials=[\"air\", \"water-liquid\", \"water-vapor\"]) to create actual phase-1/2/3 domains and verify material assignments. For an existing three-phase model, fluentagi.assign_multiphase_materials(materials=[...], directory=task_directory) assigns materials without changing the phase count. Then call fluentagi.configure_evaporation_condensation(directory=task_directory, saturation_temperature=T_sat_K, evaporation_frequency=from_frequency_per_second, condensation_frequency=to_frequency_per_second, from_phase=\"phase-2\", to_phase=\"phase-3\"). Pass the user's specified temperature/frequencies; preserve their geometry, heating and calculation parameters. This verified v242 VOF Lee adapter enables energy, uses a fixed official TUI journal and verifies the phase pair, constant saturation temperature, both frequencies and Lee model by an independent case snapshot. It does not initialize or advance the simulation. Do not say this feature is unavailable because direct TUI is forbidden; use the adapter. fluentagi.inspect_phase_change(directory=task_directory) returns actual phases and mass transfer settings, refreshing a unique case snapshot. Do not replace existing unrelated mechanisms. This adapter supports one Lee mass transfer pair, not Eulerian wall boiling, semi-mechanistic wall boiling, pressure-dependent saturation tables or UDFs. Do not claim a complete validated boiling simulation from successful setup alone. initialize_air is a TWO-PHASE adapter; do not use it for three-phase cases. Use verified settings initialization and phase-aware patching only for requested new calculations.\nThe runtime provides fluentagi.assign_phase_materials(primary=\"air\", secondary=\"water-liquid\", directory=task_directory), fluentagi.inspect_phases(), and fluentagi.export_results(directory=task_directory, fields=[\"pressure\", \"velocity-magnitude\"]). For requested animation of an already initialized transient solution use fluentagi.record_animation(directory=task_directory, field=\"velocity-magnitude\", frames=10, steps_per_frame=1, max_iter_per_step=20); it advances the solution and creates PNG frames and GIF. Never initialize or advance an existing solution without the user requesting calculation. These are executable verified adapters, not prose instructions. Use the phase adapter when asked to assign materials; do not ask the user to click the phase dialog. Print returned results. For postprocessing use export_results and assess its errors; never claim missing images were saved. Only import math/json/itertools/functools/collections/dataclasses/typing; datetime/os/pathlib imports are unavailable. Check is_active() before querying model-dependent settings on an empty mesh.\nFor NEW planar geometry and meshing use mesh = fluentagi.build_planar(directory=task_directory, points=[[x,y],...], inlet_edges=[0], outlet_edges=[2], size=0.001). Coordinates and size are in METERS; polygon vertices ordered around its boundary; edge i joins point i to point (i+1)%N. This creates real STEP CAD and converts first-order triangular Gmsh cells into a genuine Fluent mesh with inlet/outlet/walls. Then solver.settings.file.read_mesh(file_name=mesh[\"mesh_file\"]), solver.settings.mesh.check(), configure physics, initialize, iterate, and export_results. Save current case/data before replacing loaded geometry. Do not reuse a model from previous successful construction during a repair; use its mesh_file from feedback. For curved planar CAD, use fluentagi.geometry_mesh(directory=task_directory,code=gmsh_script_string); the worker has gmsh,math,output_dir already, no imports; create OCC geometry and physical line groups named inlet,outlet,walls, export STEP, generate first-order triangular or quadrilateral mesh(2). Returned mesh_file is Fluent format; gmsh-native.msh is NOT Fluent format. 3D modeling and volume mesh conversion are now implemented. fluentagi.build_volume(directory=task_directory, shape=\"box\",length=0.1,width=0.02,height=0.02,size=0.005,mesh_type=\"tet\") creates tetrahedra; mesh_type=\"hex\" creates a structured all-hexahedron box. shape=\"cylinder\",radius=0.01 supports tetrahedra with axis along +X. Inlet is X=0 and outlet X=length. fluentagi.build_extruded(directory=task_directory,points=[[x,y],...],inlet_edges=[0],outlet_edges=[2],depth=0.01,size=0.002,mesh_type=\"tet\") extrudes a planar profile, naming lateral inlet/outlet faces; front/back faces are walls. mesh_type=\"hex-dominant\" uses recombined extruded mesh and MAY include prisms: assess returned cell_types, never call mixed cells pure hex. geometry_mesh supports arbitrary OCC volumes (boolean unions/cuts), physical SURFACE groups inlet/outlet/walls, and mesh.generate(3), first-order tet/hex/prism/pyramid. Imported STEP is not currently supported by the restricted worker. build_planar mesh_type=\"quad\" produces mapped pure quadrilaterals for valid four-sided rectangles; complex polygons can be quad/tri mixed. 2D uses triangles/quads, 3D uses tet/hex. The runtime starts or safely backs up its owned solver before switching dimension according to explicit user words. Do not request user-supplied 3D mesh for supported geometry. Save backups before replacing any loaded mesh. For 3D postprocessing create useful cut planes/isosurfaces using verified settings APIs; boundary-only contours are not an interior volume visualization. For an entire new analysis, carry out all stages rather than only inspection; collect real residual/convergence evidence and exports.\nFor water-air transient filling, call fluentagi.configure_water_air(directory=task_directory,velocity=0.05,time_step=0.001,gravity_y=-9.81,inlet=\"inlet\",outlet=\"outlet\"). This backs up and sets laminar VOF, materials, phase-aware inlet/outlet, gravity and timestep; does NOT initialize or erase existing solution. For requested NEW filling use fluentagi.initialize_air(directory=task_directory), which saves a backup, hybrid initializes and patches phase-2 volume fraction to zero across all fluid cell zones. Never initialize_air on existing results without an explicit restart request. Fluent v242 contour fields are phase-2-vof (water, only after confirming phase-2=water-liquid) and phase-1-vof (air); do not confuse them. Query real contour field.allowed_values for VOF fields. For 3D interior contours/animation use section=fluentagi.create_section(axis=\"z\",position=depth/2), then export_results(...,surfaces=[section[\"surface\"]]) or record_animation(...,surfaces=[section[\"surface\"]]). A plane section is not full volumetric rendering; report it accurately. Frames are 2..60. Each frame after the first advances steps_per_frame real time steps; final time is initial time+(frames-1)*steps_per_frame*time_step. Do not claim the pipe fills if the simulated duration is too short. Normalize typos like \"二维四面体\" by explaining 2D triangular equivalent; if depth/3D was explicitly requested, use volume tools.\nFor UNSTEADY dust motion use the separate transient DPM adapters, never track_particles (steady replay). build_dust_box(directory=task_directory) creates a 3D 40mm box with a top cylindrical nozzle (axis Y, inlet at top blowing DOWN with positive normal inlet speed) and an upper side pressure vent. Save existing case before reading its mesh_file. geometry parameters are SI and can be passed as named arguments. Choose suitable air physics; configure a real pressure outlet, do not create a sealed box with uncompensated inflow. configure_transient_dust(directory=task_directory,region_min=[.012,.003,.012],region_max=[.028,.004,.028],counts=[2,2,2],release_time=.02,release_duration=.0005,total_mass=1e-8,diameter=[1e-5,5e-5]*4,density=2500,initial_velocity=[0,0,0],gravity=[0,-9.81,0],time_step=.004,wall_behavior=\"trap\") enables actual unsteady air and one-way unsteady DPM. It creates one short native injection pulse for each seed; total_mass kg is distributed across weighted parcels. It accepts explicit points instead of a region. The entire release pulse must fit inside one physical dt. Does NOT initialize. For requested NEW cases only, initialize_transient_dust(directory=task_directory) refuses any existing valid solution. Then advance_transient_dust(directory=task_directory,until_time=.2,max_iter_per_step=200,residual_tolerance=.001) advances at most 60 actual steps per call, preferring an ABSOLUTE end time; read returned final_time and call again until target. Already reached until_time does not advance again. The small demonstration explicitly uses normalized residual tolerance .001; honor stricter user requirements and never silently relax them. The default adapter tolerance is 1e-5, which the coarse benchmark did NOT meet on its initial step. Failed per-step convergence/air mass balance/particle accounting stops with needs_review and a checkpoint; never claim success. read_transient_dust(directory=task_directory) reads actual current native particle positions, fates, masses and physical time without advancement. resume_transient_dust(directory=task_directory,checkpoint=\"latest-checkpoint.json\") backs up current case, validates hashes, restores native Case/Data including particles, and verifies actual state; never initializes. read_transient_dust_results(directory=task_directory) reads saved files offline. On continuation reuse the ORIGINAL batch directory from execution feedback for read/resume/advance; do not create another configuration merely because the desktop has a new task directory. Native output remains with the original case, while preview PNG/GIF/CSV are mirrored into the current desktop task for real-time display. Every frame is a snapshot of native transient particles, not a steady trajectory interpolation. Report deposited/trapped, escaped, in-domain, incomplete, aborted and not-yet-released parcels and actual mass budget. Caption all runs \"预先释放悬浮颗粒，非积尘再悬浮\". Particle seeds/markers represent weighted parcels, not physical particle counts or true point size. Laminar transport shows resolved advection/settling; do not claim stochastic turbulent diffusion is modeled. No verified deposited-dust detachment/adhesion/UDF resuspension adapter exists. Never add an upward initial velocity and call it resuspension. Preserve steady DPM as a distinct path.\nFor EXPLICITLY STEADY dilute solid dust ONLY use the verified v242 one-way STEADY DPM adapters, not VOF. First inspect_dpm(). On a single-phase carrier first create_dust_injection with the required density (default 2500 kg/m3) to activate actual inert materials, THEN configure_dpm(directory=task_directory,density=2500,material=\"agi-dust\",max_steps=10000) verifies the inert material density and sets tracking limit; never use solid CAD material. The v242 inert material container has an unreliable active flag/get_state; adapters enumerate named material children and read those real states instead. Never query the entire inert material container. create_dust_injection(directory=task_directory,name=\"dust\",start=[0.00001,0.003,0.01],end=[0.00001,0.017,0.01],streams=12,diameter=0.00005,mass_flow=0.0000001,velocity=[0.5,0,0],material=\"agi-dust\") creates a real group injection. Replace positions with points just INSIDE the actual inlet; SI meters, diameter meters, mass_flow TOTAL kg/s (adapter divides over streams). streams=1 creates a single injection; group uses a release line between start/end. Do not use surface injection; its v242 settings readback failed validation. set_particle_boundaries(directory=task_directory,boundaries={\"inlet\":\"escape\",\"outlet\":\"escape\",\"walls\":\"trap\"}) also supports reflect with existing restitution settings; always inspect readback. Never silently change an existing multiphase or coupled DPM model. For a requested NEW analysis, configure and solve the AIR carrier first (laminar only for suitable low Reynolds), then track_particles(directory=task_directory,injections=[\"dust\"],frames=30). This tracks native DPM trajectories, exports tracks.csv/json, native summary text, statistics and PNG/GIF. It does NOT initialize or advance the carrier. Animation is a residence-time replay of native STEADY particle tracks with simultaneous release, not a transient fluid/DPM calculation. Never use air pathlines or a continuous-phase contour as dust motion. Returned counts refer to particle streams, not physical dust counts; rates use reported mass flow. Report incomplete/aborted streams, mass/count balance and carrier convergence separately. A successful track/image is not validated collection efficiency; require mesh/physics validation for engineering conclusions. Preserve results; use a new injection name if its parameters change.\nEnd with <final_answer>Chinese explanation of the intended changes, without claiming execution success</final_answer>.\nIf essential input or an incompatible session prevents a valid script, return only <question>the specific missing input in Chinese</question>.\nAfter the desktop returns execution results, either provide a corrected script or return only <final_answer>a Chinese assessment supported by those results</final_answer>. Do not execute the same successful script again. Successful execution alone does not prove convergence.\n\nPrevious conversation and execution context (reference only; do not repeat successful scripts):\n[{\"user\": \"创建长 0.2 m、高 0.02 m 的二维流道，通过 build_planar 生成 STEP 和尺寸 0.001 m 的三角形 Fluent 网格。空气层流，入口速度 0.1 m/s，出口表压 0 Pa，上下壁面无滑移。分批迭代检查收敛，保存 case/data。\"}, {\"assistant\": \"找不到输入框；请完成登录/真人验证，或在设置中更新网页选择器。\", \"run_directory\": \"C:\\\\Users\\\\13977\\\\AppData\\\\Local\\\\FluentAGI\\\\data\\\\runs\\\\20261018-130631-f68176\"}, {\"user\": \"继续\"}, {\"tool\": \"run_code\", \"result\": \"{\\\"status\\\": \\\"ok\\\", \\\"stdout\\\": \\\"\\\\nOpening input/output transcript to file \\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-130707-27e2af\\\\\\\\channel_velocity_repair.trn\\\\\\\".\\\\n\\\\n Domain Extents:\\\\n   x-coordinate: min (m) = 0.000000e+00, max (m) = 2.000000e-01\\\\n   y-coordinate: min (m) = 0.000000e+00, max (m) = 2.000000e-02\\\\n Volume statistics:\\\\n   minimum volume (m3): 2.695799e-07\\\\n   maximum volume (m3): 5.611842e-07\\\\n     total volume (m3): 4.000000e-03\\\\n Face area statistics:\\\\n\\n…中间日志已省略，完整日志保存在任务目录…\\n       9258 cells,     1 zone  ...\\\\n       14107 faces,     4 zones ...\\\\n        4850 nodes,     1 zone  ...\\\\n  Done.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-130707-27e2af\\\\\\\\channel_velocity_repair_final.dat.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\n  Writing results.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-130707-27e2af\\\\\\\\post-130923-6f2c\\\\\\\\result.cas.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\nGrouping cells for Laplace smoothing ...\\\\n        9258 cells,     1 zone  ...\\\\n       14107 faces,     4 zones ...\\\\n        4850 nodes,     1 zone  ...\\\\n  Done.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-130707-27e2af\\\\\\\\post-130923-6f2c\\\\\\\\result.dat.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\n  Writing results.\\\\nDone.\\\\nCreating zone surface for fluid zone\\\\nEXPORT_RESULTS {'status': 'ok', 'directory': 'C:\\\\\\\\\\\\\\\\Users\\\\\\\\\\\\\\\\13977\\\\\\\\\\\\\\\\AppData\\\\\\\\\\\\\\\\Local\\\\\\\\\\\\\\\\FluentAGI\\\\\\\\\\\\\\\\data\\\\\\\\\\\\\\\\runs\\\\\\\\\\\\\\\\20261018-130707-27e2af\\\\\\\\\\\\\\\\post-130923-6f2c', 'created': '2026-10-18T13:09:23.686944', 'files': ['mesh.png', 'pressure.png', 'residual.csv', 'result.cas.h5', 'result.dat.h5', 'velocity-magnitude.png'], 'errors': [], 'convergence_verified': False}\\\\n实际残差和收敛提示记录在 channel_velocity_repair.trn；请结合各批日志判断收敛，导出文件以适配器实际返回结果为准。\\\\n\\\\nTranscript closed.\\\\n\\\", \\\"stderr\\\": \\\"\\\", \\\"return_value\\\": null, \\\"message\\\": null, \\\"error_code\\\": null, \\\"warnings\\\": []}\"}, {\"assistant\": \"本次已完成计算与保存，无需重复运行。\\n\\n网格：9258 个三角形单元，4850 个节点。\\n最终第 36 次迭代，Fluent 明确提示“solution is converged”，达到当前设置的残差判据。\\n最终残差：连续性 3.4656×10⁻⁴，x 速度 3.9597×10⁻⁶，y 速度 1.5044×10⁻⁷。\\n已保存最终 case/data：channel_velocity_repair_final.cas.h5、channel_velocity_repair_final.dat.h5。\\n后处理目录 post-130923-6f2c 已导出网格图、压力图、速度图和 residual.csv，返回错误列表为空。\\n\\n上述证据说明当前残差判据已满足；质量守恒误差和网格无关性尚未验证。\", \"run_directory\": \"C:\\\\Users\\\\13977\\\\AppData\\\\Local\\\\FluentAGI\\\\data\\\\runs\\\\20261018-130707-27e2af\"}, {\"user\": \"翼型绕流，也来一个，要求智能加密网格，自己定义，要求速度算快点，我现在在演示\"}]\nRuntime capabilities:\n{\"protocol\": \"FluentAGI-capabilities-v1\", \"session\": {\"connected\": true, \"mode\": \"launch\"}, \"geometry\": {\"worker\": \"gmsh isolated process\", \"imports\": [], \"builtins\": [\"range\", \"len\", \"int\", \"float\", \"str\", \"list\", \"tuple\", \"enumerate\", \"zip\", \"min\", \"max\", \"abs\", \"round\", \"RuntimeError\", \"ValueError\", \"print\", \"set\", \"sum\", \"sorted\", \"bool\", \"all\", \"any\"], \"physical_groups\": [\"inlet\", \"outlet\", \"walls\"], \"cell_types\": [\"triangle\", \"quadrilateral\", \"tetrahedron\", \"hexahedron\", \"prism\", \"pyramid\"]}, \"script\": {\"imports\": [\"math\", \"json\", \"itertools\", \"functools\", \"collections\", \"dataclasses\", \"typing\"], \"adapters\": [\"build_dust_box\", \"configure_transient_dust\", \"initialize_transient_dust\", \"read_transient_dust\", \"advance_transient_dust\", \"resume_transient_dust\", \"read_transient_dust_results\", \"inspect_dpm\", \"configure_dpm\", \"create_dust_injection\", \"set_particle_boundaries\", \"track_particles\", \"build_planar\", \"build_volume\", \"build_extruded\", \"geometry_mesh\", \"configure_water_air\", \"initialize_air\", \"record_animation\", \"export_results\", \"assign_phase_materials\", \"assign_multiphase_materials\", \"configure_three_phase_materials\", \"audit_multiphase_interfaces\", \"configure_evaporation_condensation\", \"inspect_phase_change\", \"configure_surface_tension\", \"inspect_surface_tension\"]}, \"generated_at\": 1792300295.565992, \"phase_change\": {\"version\": \"v242\", \"model\": \"Lee\", \"adapter_multiphase_models\": [\"vof\"], \"mixture_officially_available\": true, \"mixture_adapter_validated\": false, \"two_phase_2d_correction_runtime_validation\": \"pending\", \"automatic_model_switch\": false, \"phases\": [2, 3], \"saturation\": \"constant K\", \"frequencies\": \"positive finite 1/s\", \"mass_transfer_pairs\": 1, \"internal_official_tui\": true, \"generated_direct_tui\": false, \"readback\": \"unique case snapshot\", \"initializes\": false}, \"surface_tension\": {\"version\": \"v242/v252\", \"runtime_validation\": {\"v242\": \"previous native validation\", \"v252\": \"official command and generated SDK checked; customer runtime readback required\"}, \"model\": \"VOF\", \"coefficient\": \"nonnegative finite N/m\", \"preserves_other_pairs\": true, \"readback\": \"unique case snapshot\", \"initializes\": false}, \"transient_dpm\": {\"version\": \"v242\", \"model\": \"unsteady single-phase carrier + transient one-way inert DPM\", \"release\": \"one short native pulse per explicit point / region grid, max 64 weighted parcels\", \"chunk_steps\": 60, \"positions\": \"native current positions at actual physical time; never steady replay\", \"checkpoint\": \"unique Case/Data plus SHA256 and particle-state readback\", \"acceptance\": \"each-step residuals, native air mass flux, particle mass/count fate closure\", \"default_residual_tolerance\": 1e-05, \"benchmark_residual_tolerance\": 0.001, \"strict_1e_5_initial_step_validated\": false, \"resuspension_validated\": false, \"stochastic_turbulent_dispersion_validated\": false}, \"dpm\": {\"version\": \"v242\", \"carrier\": \"single phase, one-way, steady inert dust\", \"injection_types\": [\"single\", \"group\"], \"surface_injection_validated\": false, \"boundary_types\": [\"reflect\", \"trap\", \"escape\"], \"trajectory_source\": \"native GetParticleTracksField RPC\", \"animation\": \"steady DPM trajectory residence-time replay, no carrier advance\", \"transient_dpm_validated\": false, \"two_way_validated\": false, \"readback\": true, \"active\": true}, \"fluent_version\": \"Ansys Fluent 2024 R2\", \"model_active\": true}\nCurrent session:\n{\"connected\": true, \"dimension\": 2, \"mode\": \"solver\", \"owned\": true, \"continuation\": true}\nTask directory:\nC:\\Users\\13977\\AppData\\Local\\FluentAGI\\data\\runs\\20261018-131135-2f3559\nCurrent request:\n翼型绕流，也来一个，要求智能加密网格，自己定义，要求速度算快点，我现在在演示\nDesktop execution feedback:\n[{\"failed_action\": {\"tool\": \"run_code\", \"arguments\": {\"code\": \"# Use the existing connected PyFluent variable solver.\\ntask_directory = r\\\"C:\\\\Users\\\\13977\\\\AppData\\\\Local\\\\FluentAGI\\\\data\\\\runs\\\\20261018-131135-2f3559\\\"\\nsettings = solver.settings\\ntranscript_started = False\\n\\ngmsh_code = \\\"\\\"\\\"\\ngmsh.model.add(\\\"naca0012_fast_demo\\\")\\nocc = gmsh.model.occ\\nchord = 0.1\\nn = 36\\nupper = []\\nlower = []\\nfor i in range(n + 1):\\n    x = 0.5 * (1.0 - math.cos(math.pi * i / n))\\n    yt = 5.0 * 0.12 * (\\n        0.2969 * math.sqrt(x)\\n        - 0.1260 * x\\n        - 0.3516 * x * x\\n        + 0.2843 * x * x * x\\n        - 0.1036 * x * x * x * x\\n    )\\n    if i == 0 or i == n:\\n        p = occ.addPoint(chord * x, 0.0, 0.0)\\n        upper.append(p)\\n        lower.append(p)\\n    else:\\n        upper.append(occ.addPoint(chord * x, chord * yt, 0.0))\\n        lower.append(occ.addPoint(chord * x, -chord * yt, 0.0))\\n\\ncu = occ.addSpline(upper)\\ncl = occ.addSpline(list(reversed(lower)))\\nfoil_loop = occ.addCurveLoop([cu, cl])\\np0 = occ.addPoint(-0.3, -0.3, 0)\\np1 = occ.addPoint(0.7, -0.3, 0)\\np2 = occ.addPoint(0.7, 0.3, 0)\\np3 = occ.addPoint(-0.3, 0.3, 0)\\nbottom = occ.addLine(p0, p1)\\nright = occ.addLine(p1, p2)\\ntop = occ.addLine(p2, p3)\\nleft = occ.addLine(p3, p0)\\nouter_loop = occ.addCurveLoop([bottom, right, top, left])\\nfluid = occ.addPlaneSurface([outer_loop, foil_loop])\\nocc.synchronize()\\n\\nfor name, curves in [\\n    (\\\"inlet\\\", [left]),\\n    (\\\"outlet\\\", [right]),\\n    (\\\"walls\\\", [bottom, top, cu, cl]),\\n]:\\n    tag = gmsh.model.addPhysicalGroup(1, curves)\\n    gmsh.model.setPhysicalName(1, tag, name)\\ntag = gmsh.model.addPhysicalGroup(2, [fluid])\\ngmsh.model.setPhysicalName(2, tag, \\\"fluid\\\")\\n\\ndistance = gmsh.model.mesh.field.add(\\\"Distance\\\")\\ngmsh.model.mesh.field.setNumbers(distance, \\\"CurvesList\\\", [cu, cl])\\ngmsh.model.mesh.field.setNumber(distance, \\\"Sampling\\\", 160)\\nnear = gmsh.model.mesh.field.add(\\\"Threshold\\\")\\ngmsh.model.mesh.field.setNumber(near, \\\"InField\\\", distance)\\ngmsh.model.mesh.field.setNumber(near, \\\"SizeMin\\\", 0.0008)\\ngmsh.model.mesh.field.setNumber(near, \\\"SizeMax\\\", 0.025)\\ngmsh.model.mesh.field.setNumber(near, \\\"DistMin\\\", 0.003)\\ngmsh.model.mesh.field.setNumber(near, \\\"DistMax\\\", 0.08)\\n\\nwake = gmsh.model.mesh.field.add(\\\"Box\\\")\\nfor key, value in [\\n    (\\\"VIn\\\", 0.004), (\\\"VOut\\\", 0.025),\\n    (\\\"XMin\\\", 0.085), (\\\"XMax\\\", 0.4),\\n    (\\\"YMin\\\", -0.025), (\\\"YMax\\\", 0.025),\\n    (\\\"ZMin\\\", -0.001), (\\\"ZMax\\\", 0.001),\\n    (\\\"Thickness\\\", 0.025),\\n]:\\n    gmsh.model.mesh.field.setNumber(wake, key, value)\\ncombined = gmsh.model.mesh.field.add(\\\"Min\\\")\\ngmsh.model.mesh.field.setNumbers(combined, \\\"FieldsList\\\", [near, wake])\\ngmsh.model.mesh.field.setAsBackgroundMesh(combined)\\ngmsh.option.setNumber(\\\"Mesh.MeshSizeFromPoints\\\", 0)\\ngmsh.option.setNumber(\\\"Mesh.MeshSizeFromCurvature\\\", 0)\\ngmsh.option.setNumber(\\\"Mesh.MeshSizeExtendFromBoundary\\\", 0)\\ngmsh.option.setNumber(\\\"Mesh.MeshSizeMin\\\", 0.0006)\\ngmsh.option.setNumber(\\\"Mesh.MeshSizeMax\\\", 0.025)\\ngmsh.option.setNumber(\\\"Mesh.ElementOrder\\\", 1)\\ngmsh.option.setNumber(\\\"Mesh.Algorithm\\\", 6)\\ngmsh.write(output_dir + \\\"/naca0012.step\\\")\\ngmsh.model.mesh.generate(2)\\ngmsh.model.mesh.optimize(\\\"Relocate2D\\\")\\n\\\"\\\"\\\"\\n\\ntry:\\n    settings.file.start_transcript(\\n        file_name=task_directory + r\\\"\\\\airfoil_demo.trn\\\"\\n    )\\n    transcript_started = True\\n\\n    if settings.setup.models.is_active():\\n        settings.file.write_case_data(\\n            file_name=task_directory + r\\\"\\\\previous_channel_backup.cas.h5\\\"\\n        )\\n\\n    mesh = fluentagi.geometry_mesh(\\n        directory=task_directory,\\n        code=gmsh_code,\\n    )\\n    print(\\\"AIRFOIL_MESH\\\", mesh)\\n    settings.file.read_mesh(file_name=mesh[\\\"mesh_file\\\"])\\n    settings.mesh.check()\\n\\n    if not settings.setup.models.is_active():\\n        raise RuntimeError(\\\"翼型网格读取后模型未激活。\\\")\\n\\n    settings.setup.general.solver.type = \\\"pressure-based\\\"\\n    settings.setup.general.solver.time = \\\"steady\\\"\\n    settings.setup.models.viscous.model = \\\"laminar\\\"\\n    settings.setup.models.energy.enabled = False\\n    settings.setup.general.operating_conditions.gravity.enable = False\\n\\n    air = settings.setup.materials.fluid[\\\"air\\\"]\\n    air.density.set_state({\\\"option\\\": \\\"constant\\\", \\\"value\\\": 1.225})\\n    air.viscosity.set_state({\\\"option\\\": \\\"constant\\\", \\\"value\\\": 1.7894e-5})\\n    print(\\\"AIR\\\", air.get_state())\\n    print(\\\"DEMO_PARAMETERS\\\", {\\n        \\\"airfoil\\\": \\\"NACA0012\\\",\\n        \\\"chord_m\\\": 0.1,\\n        \\\"velocity_m_s\\\": 0.1,\\n        \\\"angle_deg\\\": 0.0,\\n        \\\"Re_chord\\\": 1.225 * 0.1 * 0.1 / 1.7894e-5,\\n        \\\"model\\\": \\\"steady laminar\\\",\\n        \\\"refinement\\\": \\\"prescribed distance and wake fields\\\",\\n    })\\n\\n    zones = settings.setup.cell_zone_conditions.fluid\\n    for name in zones.get_object_names():\\n        zones[name].general.material = \\\"air\\\"\\n\\n    boundaries = settings.setup.boundary_conditions\\n    inlet = boundaries.velocity_inlet[\\\"inlet\\\"]\\n    inlet.momentum.velocity_specification_method = \\\"Magnitude, Normal to Boundary\\\"\\n    inlet.momentum.velocity.set_state({\\\"option\\\": \\\"value\\\", \\\"value\\\": 0.1})\\n    outlet = boundaries.pressure_outlet[\\\"outlet\\\"]\\n    outlet.momentum.gauge_pressure.set_state(\\n        {\\\"option\\\": \\\"value\\\", \\\"value\\\": 0.0}\\n    )\\n    for name in boundaries.wall.get_object_names():\\n        wall = boundaries.wall[name]\\n        wall.momentum.wall_motion = \\\"Stationary Wall\\\"\\n        wall.momentum.shear_condition = \\\"No Slip\\\"\\n\\n    print(\\\"INLET\\\", inlet.get_state())\\n    print(\\\"OUTLET\\\", outlet.get_state())\\n    print(\\\"WALLS\\\", boundaries.wall.get_state())\\n    print(\\\"RESIDUAL_SETTINGS\\\", settings.solution.monitor.residual.get_state())\\n\\n    settings.file.write_case(\\n        file_name=task_directory + r\\\"\\\\airfoil_configured.cas.h5\\\"\\n    )\\n    settings.solution.initialization.hybrid_initialize()\\n\\n    for batch in range(1, 4):\\n        print(\\\"BATCH_BEGIN\\\", batch, \\\"MAX_ITERATIONS\\\", 100)\\n        settings.solution.run_calculation.iterate(iter_count=100)\\n        print(\\\"BATCH_END\\\", batch)\\n        settings.file.write_case_data(\\n            file_name=task_directory\\n            + r\\\"\\\\airfoil_batch_\\\"\\n            + str(batch)\\n            + \\\".cas.h5\\\"\\n        )\\n\\n    settings.file.write_case_data(\\n        file_name=task_directory + r\\\"\\\\airfoil_final.cas.h5\\\"\\n    )\\n    result = fluentagi.export_results(\\n        directory=task_directory,\\n        fields=[\\\"pressure\\\", \\\"velocity-magnitude\\\"],\\n    )\\n    print(\\\"EXPORT_RESULTS\\\", result)\\n    print(\\n        \\\"本案例为低雷诺数零攻角风洞演示，采用预设空间局部加密，\\\"\\n        \\\"不是基于求解误差的自适应网格。\\\"\\n        \\\"实际收敛需核对 airfoil_demo.trn 和导出的 residual.csv；\\\"\\n        \\\"若未达到判据，保留当前解继续迭代，不重新初始化。\\\"\\n    )\\n\\nfinally:\\n    if transcript_started:\\n        settings.file.stop_transcript()\"}}, \"error\": \"{\\\"status\\\": \\\"error\\\", \\\"stdout\\\": \\\"\\\\nOpening input/output transcript to file \\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\airfoil_demo.trn\\\\\\\".\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\previous_channel_backup.cas.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\nGrouping cells for Laplace smoothing ...\\\\n        9258 cells,     1 zone  ...\\\\n       14107 faces,     4 zones ...\\\\n        4850 nodes,     1 zone  ...\\\\n  Done.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\previous_channel_backup.dat.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\n  Writing results.\\\\nDone.\\\\n\\\\n\\\", \\\"stderr\\\": \\\"\\\\nTraceback (most recent call last):\\\\n  File \\\\\\\"ansys\\\\\\\\fluent\\\\\\\\mcp\\\\\\\\solve\\\\\\\\backends\\\\\\\\pyfluent.py\\\\\\\", line 2793, in _do\\\\n    exec(  # noqa: S102  # nosec B102\\\\n  File \\\\\\\"<mcp>\\\\\\\", line 100, in <module>\\\\n  File \\\\\\\"automation.py\\\\\\\", line 84, in geometry_mesh\\\\n  File \\\\\\\"geometry.py\\\\\\\", line 21, in run_geometry\\\\n  File \\\\\\\"geometry.py\\\\\\\", line 15, in validate_geometry\\\\nValueError: 不允许的名称：reversed\\\\n\\\", \\\"return_value\\\": null, \\\"message\\\": \\\"不允许的名称：reversed\\\", \\\"error_code\\\": \\\"execution_error\\\", \\\"warnings\\\": []}\", \"note\": \"可能有部分操作已生效，请先检查实时状态，修复后继续。\"}]",
      "reply": "ChatGPT 说：\n\n失败原因是几何工作器不允许 reversed；改用切片倒序。原流道已备份、翼型尚未生成，本轮继续完整建模和计算。\n\n<fluent_code>\n```python\n# Use the existing connected PyFluent variable solver.\ntask_directory = r\"C:\\Users\\13977\\AppData\\Local\\FluentAGI\\data\\runs\\20261018-131135-2f3559\"\nsettings = solver.settings\ntranscript_started = False\n\ngmsh_code = \"\"\"\ngmsh.model.add(\"naca0012_fast_repair\")\nocc = gmsh.model.occ\nchord = 0.1\nn = 36\nupper = []\nlower = []\nfor i in range(n + 1):\n    x = 0.5 * (1.0 - math.cos(math.pi * i / n))\n    yt = 0.6 * (\n        0.2969 * math.sqrt(x)\n        - 0.1260 * x\n        - 0.3516 * x * x\n        + 0.2843 * x * x * x\n        - 0.1036 * x * x * x * x\n    )\n    if i == 0 or i == n:\n        p = occ.addPoint(chord * x, 0.0, 0.0)\n        upper.append(p)\n        lower.append(p)\n    else:\n        upper.append(occ.addPoint(chord * x, chord * yt, 0.0))\n        lower.append(occ.addPoint(chord * x, -chord * yt, 0.0))\ncu = occ.addSpline(upper)\ncl = occ.addSpline(lower[::-1])\nfoil_loop = occ.addCurveLoop([cu, cl])\n\np0 = occ.addPoint(-0.3, -0.3, 0)\np1 = occ.addPoint(0.7, -0.3, 0)\np2 = occ.addPoint(0.7, 0.3, 0)\np3 = occ.addPoint(-0.3, 0.3, 0)\nbottom = occ.addLine(p0, p1)\nright = occ.addLine(p1, p2)\ntop = occ.addLine(p2, p3)\nleft = occ.addLine(p3, p0)\nouter_loop = occ.addCurveLoop([bottom, right, top, left])\nfluid = occ.addPlaneSurface([outer_loop, foil_loop])\nocc.synchronize()\n\nfor name, curves in [\n    (\"inlet\", [left]),\n    (\"outlet\", [right]),\n    (\"walls\", [bottom, top, cu, cl]),\n]:\n    tag = gmsh.model.addPhysicalGroup(1, curves)\n    gmsh.model.setPhysicalName(1, tag, name)\ntag = gmsh.model.addPhysicalGroup(2, [fluid])\ngmsh.model.setPhysicalName(2, tag, \"fluid\")\n\ndistance = gmsh.model.mesh.field.add(\"Distance\")\ngmsh.model.mesh.field.setNumbers(distance, \"CurvesList\", [cu, cl])\ngmsh.model.mesh.field.setNumber(distance, \"Sampling\", 160)\nnear = gmsh.model.mesh.field.add(\"Threshold\")\nfor key, value in [\n    (\"InField\", distance),\n    (\"SizeMin\", 0.0008),\n    (\"SizeMax\", 0.025),\n    (\"DistMin\", 0.003),\n    (\"DistMax\", 0.08),\n]:\n    gmsh.model.mesh.field.setNumber(near, key, value)\n\nwake = gmsh.model.mesh.field.add(\"Box\")\nfor key, value in [\n    (\"VIn\", 0.004), (\"VOut\", 0.025),\n    (\"XMin\", 0.085), (\"XMax\", 0.4),\n    (\"YMin\", -0.025), (\"YMax\", 0.025),\n    (\"ZMin\", -0.001), (\"ZMax\", 0.001),\n    (\"Thickness\", 0.025),\n]:\n    gmsh.model.mesh.field.setNumber(wake, key, value)\ncombined = gmsh.model.mesh.field.add(\"Min\")\ngmsh.model.mesh.field.setNumbers(combined, \"FieldsList\", [near, wake])\ngmsh.model.mesh.field.setAsBackgroundMesh(combined)\n\nfor key, value in [\n    (\"Mesh.MeshSizeFromPoints\", 0),\n    (\"Mesh.MeshSizeFromCurvature\", 0),\n    (\"Mesh.MeshSizeExtendFromBoundary\", 0),\n    (\"Mesh.MeshSizeMin\", 0.0006),\n    (\"Mesh.MeshSizeMax\", 0.025),\n    (\"Mesh.ElementOrder\", 1),\n    (\"Mesh.Algorithm\", 6),\n]:\n    gmsh.option.setNumber(key, value)\ngmsh.write(output_dir + \"/naca0012.step\")\ngmsh.model.mesh.generate(2)\ngmsh.model.mesh.optimize(\"Relocate2D\")\n\"\"\"\n\ntry:\n    settings.file.start_transcript(\n        file_name=task_directory + r\"\\airfoil_repair.trn\"\n    )\n    transcript_started = True\n\n    if settings.setup.models.is_active():\n        print(\"CURRENT_MODELS\", settings.setup.models.get_state())\n        settings.file.write_case_data(\n            file_name=task_directory + r\"\\before_airfoil_repair.cas.h5\"\n        )\n\n    mesh = fluentagi.geometry_mesh(\n        directory=task_directory,\n        code=gmsh_code,\n    )\n    print(\"AIRFOIL_MESH\", mesh)\n    settings.file.read_mesh(file_name=mesh[\"mesh_file\"])\n    settings.mesh.check()\n\n    if not settings.setup.models.is_active():\n        raise RuntimeError(\"翼型网格读入后模型未激活。\")\n\n    settings.setup.general.solver.type = \"pressure-based\"\n    settings.setup.general.solver.time = \"steady\"\n    settings.setup.models.viscous.model = \"laminar\"\n    settings.setup.models.energy.enabled = False\n    settings.setup.general.operating_conditions.gravity.enable = False\n\n    air = settings.setup.materials.fluid[\"air\"]\n    air.density.set_state({\"option\": \"constant\", \"value\": 1.225})\n    air.viscosity.set_state({\"option\": \"constant\", \"value\": 1.7894e-5})\n    print(\"AIR_READBACK\", air.get_state())\n\n    zones = settings.setup.cell_zone_conditions.fluid\n    zone_names = zones.get_object_names()\n    if not zone_names:\n        raise RuntimeError(\"没有流体单元区。\")\n    for name in zone_names:\n        zones[name].general.material = \"air\"\n\n    boundaries = settings.setup.boundary_conditions\n    inlet = boundaries.velocity_inlet[\"inlet\"]\n    inlet.momentum.velocity_specification_method = \"Magnitude, Normal to Boundary\"\n    inlet.momentum.velocity.set_state({\"option\": \"value\", \"value\": 0.1})\n    outlet = boundaries.pressure_outlet[\"outlet\"]\n    outlet.momentum.gauge_pressure.set_state(\n        {\"option\": \"value\", \"value\": 0.0}\n    )\n    for name in boundaries.wall.get_object_names():\n        wall = boundaries.wall[name]\n        wall.momentum.wall_motion = \"Stationary Wall\"\n        wall.momentum.shear_condition = \"No Slip\"\n        print(\"WALL_READBACK\", name, wall.get_state())\n\n    velocity_state = inlet.momentum.velocity.get_state()\n    pressure_state = outlet.momentum.gauge_pressure.get_state()\n    print(\"INLET_READBACK\", velocity_state)\n    print(\"OUTLET_READBACK\", pressure_state)\n    if abs(velocity_state[\"value\"] - 0.1) > 1e-10:\n        raise RuntimeError(\"入口速度读回不符。\")\n    if abs(pressure_state[\"value\"]) > 1e-10:\n        raise RuntimeError(\"出口表压读回不符。\")\n\n    print(\"RE_CHORD\", 1.225 * 0.1 * 0.1 / 1.7894e-5)\n    print(\"RESIDUAL_SETTINGS\", settings.solution.monitor.residual.get_state())\n    settings.file.write_case(\n        file_name=task_directory + r\"\\airfoil_repair_configured.cas.h5\"\n    )\n    settings.solution.initialization.hybrid_initialize()\n\n    for batch in range(1, 4):\n        print(\"BATCH_BEGIN\", batch, \"MAX_ITERATIONS\", 100)\n        settings.solution.run_calculation.iterate(iter_count=100)\n        print(\"BATCH_END\", batch)\n        settings.file.write_case_data(\n            file_name=task_directory\n            + r\"\\airfoil_repair_batch_\"\n            + str(batch)\n            + \".cas.h5\"\n        )\n\n    settings.file.write_case_data(\n        file_name=task_directory + r\"\\airfoil_repair_final.cas.h5\"\n    )\n    result = fluentagi.export_results(\n        directory=task_directory,\n        fields=[\"pressure\", \"velocity-magnitude\"],\n    )\n    print(\"EXPORT_RESULTS\", result)\n    print(\n        \"低雷诺数零攻角风洞演示；翼面距离场和尾迹区域预设加密。\"\n        \"收敛依据 airfoil_repair.trn 中实际残差和收敛提示判断，\"\n        \"导出成功与否依据 EXPORT_RESULTS 返回状态及错误列表判断。\"\n    )\n\nfinally:\n    if transcript_started:\n        settings.file.stop_transcript()\n```\n</fluent_code>\n\n<final_answer>已移除不受支持的 reversed 调用，保留翼面与尾迹局部加密及原定快速演示参数。脚本拟完成翼型网格、分批求解、case/data 保存和云图导出，实际结果等待执行反馈确认。</final_answer>",
      "executed_script": "# Use the existing connected PyFluent variable solver.\ntask_directory = r\"C:\\Users\\13977\\AppData\\Local\\FluentAGI\\data\\runs\\20261018-131135-2f3559\"\nsettings = solver.settings\ntranscript_started = False\n\ngmsh_code = \"\"\"\ngmsh.model.add(\"naca0012_fast_repair\")\nocc = gmsh.model.occ\nchord = 0.1\nn = 36\nupper = []\nlower = []\nfor i in range(n + 1):\n    x = 0.5 * (1.0 - math.cos(math.pi * i / n))\n    yt = 0.6 * (\n        0.2969 * math.sqrt(x)\n        - 0.1260 * x\n        - 0.3516 * x * x\n        + 0.2843 * x * x * x\n        - 0.1036 * x * x * x * x\n    )\n    if i == 0 or i == n:\n        p = occ.addPoint(chord * x, 0.0, 0.0)\n        upper.append(p)\n        lower.append(p)\n    else:\n        upper.append(occ.addPoint(chord * x, chord * yt, 0.0))\n        lower.append(occ.addPoint(chord * x, -chord * yt, 0.0))\ncu = occ.addSpline(upper)\ncl = occ.addSpline(lower[::-1])\nfoil_loop = occ.addCurveLoop([cu, cl])\n\np0 = occ.addPoint(-0.3, -0.3, 0)\np1 = occ.addPoint(0.7, -0.3, 0)\np2 = occ.addPoint(0.7, 0.3, 0)\np3 = occ.addPoint(-0.3, 0.3, 0)\nbottom = occ.addLine(p0, p1)\nright = occ.addLine(p1, p2)\ntop = occ.addLine(p2, p3)\nleft = occ.addLine(p3, p0)\nouter_loop = occ.addCurveLoop([bottom, right, top, left])\nfluid = occ.addPlaneSurface([outer_loop, foil_loop])\nocc.synchronize()\n\nfor name, curves in [\n    (\"inlet\", [left]),\n    (\"outlet\", [right]),\n    (\"walls\", [bottom, top, cu, cl]),\n]:\n    tag = gmsh.model.addPhysicalGroup(1, curves)\n    gmsh.model.setPhysicalName(1, tag, name)\ntag = gmsh.model.addPhysicalGroup(2, [fluid])\ngmsh.model.setPhysicalName(2, tag, \"fluid\")\n\ndistance = gmsh.model.mesh.field.add(\"Distance\")\ngmsh.model.mesh.field.setNumbers(distance, \"CurvesList\", [cu, cl])\ngmsh.model.mesh.field.setNumber(distance, \"Sampling\", 160)\nnear = gmsh.model.mesh.field.add(\"Threshold\")\nfor key, value in [\n    (\"InField\", distance),\n    (\"SizeMin\", 0.0008),\n    (\"SizeMax\", 0.025),\n    (\"DistMin\", 0.003),\n    (\"DistMax\", 0.08),\n]:\n    gmsh.model.mesh.field.setNumber(near, key, value)\n\nwake = gmsh.model.mesh.field.add(\"Box\")\nfor key, value in [\n    (\"VIn\", 0.004), (\"VOut\", 0.025),\n    (\"XMin\", 0.085), (\"XMax\", 0.4),\n    (\"YMin\", -0.025), (\"YMax\", 0.025),\n    (\"ZMin\", -0.001), (\"ZMax\", 0.001),\n    (\"Thickness\", 0.025),\n]:\n    gmsh.model.mesh.field.setNumber(wake, key, value)\ncombined = gmsh.model.mesh.field.add(\"Min\")\ngmsh.model.mesh.field.setNumbers(combined, \"FieldsList\", [near, wake])\ngmsh.model.mesh.field.setAsBackgroundMesh(combined)\n\nfor key, value in [\n    (\"Mesh.MeshSizeFromPoints\", 0),\n    (\"Mesh.MeshSizeFromCurvature\", 0),\n    (\"Mesh.MeshSizeExtendFromBoundary\", 0),\n    (\"Mesh.MeshSizeMin\", 0.0006),\n    (\"Mesh.MeshSizeMax\", 0.025),\n    (\"Mesh.ElementOrder\", 1),\n    (\"Mesh.Algorithm\", 6),\n]:\n    gmsh.option.setNumber(key, value)\ngmsh.write(output_dir + \"/naca0012.step\")\ngmsh.model.mesh.generate(2)\ngmsh.model.mesh.optimize(\"Relocate2D\")\n\"\"\"\n\ntry:\n    settings.file.start_transcript(\n        file_name=task_directory + r\"\\airfoil_repair.trn\"\n    )\n    transcript_started = True\n\n    if settings.setup.models.is_active():\n        print(\"CURRENT_MODELS\", settings.setup.models.get_state())\n        settings.file.write_case_data(\n            file_name=task_directory + r\"\\before_airfoil_repair.cas.h5\"\n        )\n\n    mesh = fluentagi.geometry_mesh(\n        directory=task_directory,\n        code=gmsh_code,\n    )\n    print(\"AIRFOIL_MESH\", mesh)\n    settings.file.read_mesh(file_name=mesh[\"mesh_file\"])\n    settings.mesh.check()\n\n    if not settings.setup.models.is_active():\n        raise RuntimeError(\"翼型网格读入后模型未激活。\")\n\n    settings.setup.general.solver.type = \"pressure-based\"\n    settings.setup.general.solver.time = \"steady\"\n    settings.setup.models.viscous.model = \"laminar\"\n    settings.setup.models.energy.enabled = False\n    settings.setup.general.operating_conditions.gravity.enable = False\n\n    air = settings.setup.materials.fluid[\"air\"]\n    air.density.set_state({\"option\": \"constant\", \"value\": 1.225})\n    air.viscosity.set_state({\"option\": \"constant\", \"value\": 1.7894e-5})\n    print(\"AIR_READBACK\", air.get_state())\n\n    zones = settings.setup.cell_zone_conditions.fluid\n    zone_names = zones.get_object_names()\n    if not zone_names:\n        raise RuntimeError(\"没有流体单元区。\")\n    for name in zone_names:\n        zones[name].general.material = \"air\"\n\n    boundaries = settings.setup.boundary_conditions\n    inlet = boundaries.velocity_inlet[\"inlet\"]\n    inlet.momentum.velocity_specification_method = \"Magnitude, Normal to Boundary\"\n    inlet.momentum.velocity.set_state({\"option\": \"value\", \"value\": 0.1})\n    outlet = boundaries.pressure_outlet[\"outlet\"]\n    outlet.momentum.gauge_pressure.set_state(\n        {\"option\": \"value\", \"value\": 0.0}\n    )\n    for name in boundaries.wall.get_object_names():\n        wall = boundaries.wall[name]\n        wall.momentum.wall_motion = \"Stationary Wall\"\n        wall.momentum.shear_condition = \"No Slip\"\n        print(\"WALL_READBACK\", name, wall.get_state())\n\n    velocity_state = inlet.momentum.velocity.get_state()\n    pressure_state = outlet.momentum.gauge_pressure.get_state()\n    print(\"INLET_READBACK\", velocity_state)\n    print(\"OUTLET_READBACK\", pressure_state)\n    if abs(velocity_state[\"value\"] - 0.1) > 1e-10:\n        raise RuntimeError(\"入口速度读回不符。\")\n    if abs(pressure_state[\"value\"]) > 1e-10:\n        raise RuntimeError(\"出口表压读回不符。\")\n\n    print(\"RE_CHORD\", 1.225 * 0.1 * 0.1 / 1.7894e-5)\n    print(\"RESIDUAL_SETTINGS\", settings.solution.monitor.residual.get_state())\n    settings.file.write_case(\n        file_name=task_directory + r\"\\airfoil_repair_configured.cas.h5\"\n    )\n    settings.solution.initialization.hybrid_initialize()\n\n    for batch in range(1, 4):\n        print(\"BATCH_BEGIN\", batch, \"MAX_ITERATIONS\", 100)\n        settings.solution.run_calculation.iterate(iter_count=100)\n        print(\"BATCH_END\", batch)\n        settings.file.write_case_data(\n            file_name=task_directory\n            + r\"\\airfoil_repair_batch_\"\n            + str(batch)\n            + \".cas.h5\"\n        )\n\n    settings.file.write_case_data(\n        file_name=task_directory + r\"\\airfoil_repair_final.cas.h5\"\n    )\n    result = fluentagi.export_results(\n        directory=task_directory,\n        fields=[\"pressure\", \"velocity-magnitude\"],\n    )\n    print(\"EXPORT_RESULTS\", result)\n    print(\n        \"低雷诺数零攻角风洞演示；翼面距离场和尾迹区域预设加密。\"\n        \"收敛依据 airfoil_repair.trn 中实际残差和收敛提示判断，\"\n        \"导出成功与否依据 EXPORT_RESULTS 返回状态及错误列表判断。\"\n    )\n\nfinally:\n    if transcript_started:\n        settings.file.stop_transcript()"
    },
    {
      "round": "round-03",
      "prompt": "You are FluentAGI for Ansys Fluent. Write one short Chinese plan, then a single COMPLETE Python script in this exact Markdown layout:\n\n<fluent_code>\n\n```python\n# Use the existing connected PyFluent variable solver.\n# Continue with the complete executable script here.\n```\n\n</fluent_code>\n\nPut a newline before and after each tag and each fence. Put no prose, headings, units, or explanations inside the fenced Python block. Do not place ```python and Python statements on the same line. Keep the script under 280 lines. Use loops instead of repeating similar statements. Never truncate a string, parenthesis, or code fence; always close </fluent_code>.\nUse the existing solver session and compatible PyFluent APIs. A completed conversation turn does not close the session. For continuation requests reuse the loaded mesh and solution, inspect relevant current settings, and continue from actual flow time. Never launch, disconnect, remesh or initialize merely because a new desktop task directory was created. Do not launch or close Fluent. Do not use Abaqus APIs. Use solver.settings APIs and the provided fluentagi adapters. Direct solver.tui, execute_tui and Scheme remain rejected; the trusted v242 adapters may internally use fixed official TUI commands/journals. For mesh display use solver.settings.results.graphics.mesh and graphics.views APIs. Do not return JSON tool plans. Do not invent mesh files or API names. Only operate on the requested case and task directory. Preserve existing results. For a repair, inspect partially applied state and write a complete corrected script, not a patch or a repeated broken script.\nThe web AI cannot read or modify host application source. Do not claim to have searched the host disk or request uploading FluentAGI source to run simulations. Use the verified runtime adapters. Define task_directory as the absolute Task directory below before calling adapters. For VOF surface tension use fluentagi.configure_surface_tension(directory=task_directory,coefficient=0.072,phase_a=\"phase-1\",phase_b=\"phase-2\"); coefficient is N/m, replace the example with the requested value. This v242/v252 surface-tension adapter preserves other phase pairs, enables the surface-tension model and reads back every coefficient. inspect_surface_tension(directory=task_directory) returns actual state. Fluent 2025 R2 is accepted for this surface-tension adapter; do not ask to downgrade to 2024. Other Lee/DPM adapters retain their own version restrictions. Never claim v252 execution was validated before reading actual results. Do not ask the user to edit the plugin or click GUI dialogs for this supported operation.\nMixture and VOF both support Lee evaporation-condensation in official Fluent 2024 R2, but this runtime has NOT validated a Mixture configuration adapter. Do not silently substitute VOF for a Mixture tutorial or claim equivalent results. audit_multiphase_interfaces() is a read-only native settings probe, without TUI, Scheme or case writes. The VOF adapter uses narrowly scoped prompt profiles; unsupported dimension/phase combinations are rejected rather than guessed. For three-phase boiling setup in Fluent 2024 R2, use fluentagi.configure_three_phase_materials(directory=task_directory, materials=[\"air\", \"water-liquid\", \"water-vapor\"]) to create actual phase-1/2/3 domains and verify material assignments. For an existing three-phase model, fluentagi.assign_multiphase_materials(materials=[...], directory=task_directory) assigns materials without changing the phase count. Then call fluentagi.configure_evaporation_condensation(directory=task_directory, saturation_temperature=T_sat_K, evaporation_frequency=from_frequency_per_second, condensation_frequency=to_frequency_per_second, from_phase=\"phase-2\", to_phase=\"phase-3\"). Pass the user's specified temperature/frequencies; preserve their geometry, heating and calculation parameters. This verified v242 VOF Lee adapter enables energy, uses a fixed official TUI journal and verifies the phase pair, constant saturation temperature, both frequencies and Lee model by an independent case snapshot. It does not initialize or advance the simulation. Do not say this feature is unavailable because direct TUI is forbidden; use the adapter. fluentagi.inspect_phase_change(directory=task_directory) returns actual phases and mass transfer settings, refreshing a unique case snapshot. Do not replace existing unrelated mechanisms. This adapter supports one Lee mass transfer pair, not Eulerian wall boiling, semi-mechanistic wall boiling, pressure-dependent saturation tables or UDFs. Do not claim a complete validated boiling simulation from successful setup alone. initialize_air is a TWO-PHASE adapter; do not use it for three-phase cases. Use verified settings initialization and phase-aware patching only for requested new calculations.\nThe runtime provides fluentagi.assign_phase_materials(primary=\"air\", secondary=\"water-liquid\", directory=task_directory), fluentagi.inspect_phases(), and fluentagi.export_results(directory=task_directory, fields=[\"pressure\", \"velocity-magnitude\"]). For requested animation of an already initialized transient solution use fluentagi.record_animation(directory=task_directory, field=\"velocity-magnitude\", frames=10, steps_per_frame=1, max_iter_per_step=20); it advances the solution and creates PNG frames and GIF. Never initialize or advance an existing solution without the user requesting calculation. These are executable verified adapters, not prose instructions. Use the phase adapter when asked to assign materials; do not ask the user to click the phase dialog. Print returned results. For postprocessing use export_results and assess its errors; never claim missing images were saved. Only import math/json/itertools/functools/collections/dataclasses/typing; datetime/os/pathlib imports are unavailable. Check is_active() before querying model-dependent settings on an empty mesh.\nFor NEW planar geometry and meshing use mesh = fluentagi.build_planar(directory=task_directory, points=[[x,y],...], inlet_edges=[0], outlet_edges=[2], size=0.001). Coordinates and size are in METERS; polygon vertices ordered around its boundary; edge i joins point i to point (i+1)%N. This creates real STEP CAD and converts first-order triangular Gmsh cells into a genuine Fluent mesh with inlet/outlet/walls. Then solver.settings.file.read_mesh(file_name=mesh[\"mesh_file\"]), solver.settings.mesh.check(), configure physics, initialize, iterate, and export_results. Save current case/data before replacing loaded geometry. Do not reuse a model from previous successful construction during a repair; use its mesh_file from feedback. For curved planar CAD, use fluentagi.geometry_mesh(directory=task_directory,code=gmsh_script_string); the worker has gmsh,math,output_dir already, no imports; create OCC geometry and physical line groups named inlet,outlet,walls, export STEP, generate first-order triangular or quadrilateral mesh(2). Returned mesh_file is Fluent format; gmsh-native.msh is NOT Fluent format. 3D modeling and volume mesh conversion are now implemented. fluentagi.build_volume(directory=task_directory, shape=\"box\",length=0.1,width=0.02,height=0.02,size=0.005,mesh_type=\"tet\") creates tetrahedra; mesh_type=\"hex\" creates a structured all-hexahedron box. shape=\"cylinder\",radius=0.01 supports tetrahedra with axis along +X. Inlet is X=0 and outlet X=length. fluentagi.build_extruded(directory=task_directory,points=[[x,y],...],inlet_edges=[0],outlet_edges=[2],depth=0.01,size=0.002,mesh_type=\"tet\") extrudes a planar profile, naming lateral inlet/outlet faces; front/back faces are walls. mesh_type=\"hex-dominant\" uses recombined extruded mesh and MAY include prisms: assess returned cell_types, never call mixed cells pure hex. geometry_mesh supports arbitrary OCC volumes (boolean unions/cuts), physical SURFACE groups inlet/outlet/walls, and mesh.generate(3), first-order tet/hex/prism/pyramid. Imported STEP is not currently supported by the restricted worker. build_planar mesh_type=\"quad\" produces mapped pure quadrilaterals for valid four-sided rectangles; complex polygons can be quad/tri mixed. 2D uses triangles/quads, 3D uses tet/hex. The runtime starts or safely backs up its owned solver before switching dimension according to explicit user words. Do not request user-supplied 3D mesh for supported geometry. Save backups before replacing any loaded mesh. For 3D postprocessing create useful cut planes/isosurfaces using verified settings APIs; boundary-only contours are not an interior volume visualization. For an entire new analysis, carry out all stages rather than only inspection; collect real residual/convergence evidence and exports.\nFor water-air transient filling, call fluentagi.configure_water_air(directory=task_directory,velocity=0.05,time_step=0.001,gravity_y=-9.81,inlet=\"inlet\",outlet=\"outlet\"). This backs up and sets laminar VOF, materials, phase-aware inlet/outlet, gravity and timestep; does NOT initialize or erase existing solution. For requested NEW filling use fluentagi.initialize_air(directory=task_directory), which saves a backup, hybrid initializes and patches phase-2 volume fraction to zero across all fluid cell zones. Never initialize_air on existing results without an explicit restart request. Fluent v242 contour fields are phase-2-vof (water, only after confirming phase-2=water-liquid) and phase-1-vof (air); do not confuse them. Query real contour field.allowed_values for VOF fields. For 3D interior contours/animation use section=fluentagi.create_section(axis=\"z\",position=depth/2), then export_results(...,surfaces=[section[\"surface\"]]) or record_animation(...,surfaces=[section[\"surface\"]]). A plane section is not full volumetric rendering; report it accurately. Frames are 2..60. Each frame after the first advances steps_per_frame real time steps; final time is initial time+(frames-1)*steps_per_frame*time_step. Do not claim the pipe fills if the simulated duration is too short. Normalize typos like \"二维四面体\" by explaining 2D triangular equivalent; if depth/3D was explicitly requested, use volume tools.\nFor UNSTEADY dust motion use the separate transient DPM adapters, never track_particles (steady replay). build_dust_box(directory=task_directory) creates a 3D 40mm box with a top cylindrical nozzle (axis Y, inlet at top blowing DOWN with positive normal inlet speed) and an upper side pressure vent. Save existing case before reading its mesh_file. geometry parameters are SI and can be passed as named arguments. Choose suitable air physics; configure a real pressure outlet, do not create a sealed box with uncompensated inflow. configure_transient_dust(directory=task_directory,region_min=[.012,.003,.012],region_max=[.028,.004,.028],counts=[2,2,2],release_time=.02,release_duration=.0005,total_mass=1e-8,diameter=[1e-5,5e-5]*4,density=2500,initial_velocity=[0,0,0],gravity=[0,-9.81,0],time_step=.004,wall_behavior=\"trap\") enables actual unsteady air and one-way unsteady DPM. It creates one short native injection pulse for each seed; total_mass kg is distributed across weighted parcels. It accepts explicit points instead of a region. The entire release pulse must fit inside one physical dt. Does NOT initialize. For requested NEW cases only, initialize_transient_dust(directory=task_directory) refuses any existing valid solution. Then advance_transient_dust(directory=task_directory,until_time=.2,max_iter_per_step=200,residual_tolerance=.001) advances at most 60 actual steps per call, preferring an ABSOLUTE end time; read returned final_time and call again until target. Already reached until_time does not advance again. The small demonstration explicitly uses normalized residual tolerance .001; honor stricter user requirements and never silently relax them. The default adapter tolerance is 1e-5, which the coarse benchmark did NOT meet on its initial step. Failed per-step convergence/air mass balance/particle accounting stops with needs_review and a checkpoint; never claim success. read_transient_dust(directory=task_directory) reads actual current native particle positions, fates, masses and physical time without advancement. resume_transient_dust(directory=task_directory,checkpoint=\"latest-checkpoint.json\") backs up current case, validates hashes, restores native Case/Data including particles, and verifies actual state; never initializes. read_transient_dust_results(directory=task_directory) reads saved files offline. On continuation reuse the ORIGINAL batch directory from execution feedback for read/resume/advance; do not create another configuration merely because the desktop has a new task directory. Native output remains with the original case, while preview PNG/GIF/CSV are mirrored into the current desktop task for real-time display. Every frame is a snapshot of native transient particles, not a steady trajectory interpolation. Report deposited/trapped, escaped, in-domain, incomplete, aborted and not-yet-released parcels and actual mass budget. Caption all runs \"预先释放悬浮颗粒，非积尘再悬浮\". Particle seeds/markers represent weighted parcels, not physical particle counts or true point size. Laminar transport shows resolved advection/settling; do not claim stochastic turbulent diffusion is modeled. No verified deposited-dust detachment/adhesion/UDF resuspension adapter exists. Never add an upward initial velocity and call it resuspension. Preserve steady DPM as a distinct path.\nFor EXPLICITLY STEADY dilute solid dust ONLY use the verified v242 one-way STEADY DPM adapters, not VOF. First inspect_dpm(). On a single-phase carrier first create_dust_injection with the required density (default 2500 kg/m3) to activate actual inert materials, THEN configure_dpm(directory=task_directory,density=2500,material=\"agi-dust\",max_steps=10000) verifies the inert material density and sets tracking limit; never use solid CAD material. The v242 inert material container has an unreliable active flag/get_state; adapters enumerate named material children and read those real states instead. Never query the entire inert material container. create_dust_injection(directory=task_directory,name=\"dust\",start=[0.00001,0.003,0.01],end=[0.00001,0.017,0.01],streams=12,diameter=0.00005,mass_flow=0.0000001,velocity=[0.5,0,0],material=\"agi-dust\") creates a real group injection. Replace positions with points just INSIDE the actual inlet; SI meters, diameter meters, mass_flow TOTAL kg/s (adapter divides over streams). streams=1 creates a single injection; group uses a release line between start/end. Do not use surface injection; its v242 settings readback failed validation. set_particle_boundaries(directory=task_directory,boundaries={\"inlet\":\"escape\",\"outlet\":\"escape\",\"walls\":\"trap\"}) also supports reflect with existing restitution settings; always inspect readback. Never silently change an existing multiphase or coupled DPM model. For a requested NEW analysis, configure and solve the AIR carrier first (laminar only for suitable low Reynolds), then track_particles(directory=task_directory,injections=[\"dust\"],frames=30). This tracks native DPM trajectories, exports tracks.csv/json, native summary text, statistics and PNG/GIF. It does NOT initialize or advance the carrier. Animation is a residence-time replay of native STEADY particle tracks with simultaneous release, not a transient fluid/DPM calculation. Never use air pathlines or a continuous-phase contour as dust motion. Returned counts refer to particle streams, not physical dust counts; rates use reported mass flow. Report incomplete/aborted streams, mass/count balance and carrier convergence separately. A successful track/image is not validated collection efficiency; require mesh/physics validation for engineering conclusions. Preserve results; use a new injection name if its parameters change.\nEnd with <final_answer>Chinese explanation of the intended changes, without claiming execution success</final_answer>.\nIf essential input or an incompatible session prevents a valid script, return only <question>the specific missing input in Chinese</question>.\nAfter the desktop returns execution results, either provide a corrected script or return only <final_answer>a Chinese assessment supported by those results</final_answer>. Do not execute the same successful script again. Successful execution alone does not prove convergence.\n\nPrevious conversation and execution context (reference only; do not repeat successful scripts):\n[{\"user\": \"创建长 0.2 m、高 0.02 m 的二维流道，通过 build_planar 生成 STEP 和尺寸 0.001 m 的三角形 Fluent 网格。空气层流，入口速度 0.1 m/s，出口表压 0 Pa，上下壁面无滑移。分批迭代检查收敛，保存 case/data。\"}, {\"assistant\": \"找不到输入框；请完成登录/真人验证，或在设置中更新网页选择器。\", \"run_directory\": \"C:\\\\Users\\\\13977\\\\AppData\\\\Local\\\\FluentAGI\\\\data\\\\runs\\\\20261018-130631-f68176\"}, {\"user\": \"继续\"}, {\"tool\": \"run_code\", \"result\": \"{\\\"status\\\": \\\"ok\\\", \\\"stdout\\\": \\\"\\\\nOpening input/output transcript to file \\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-130707-27e2af\\\\\\\\channel_velocity_repair.trn\\\\\\\".\\\\n\\\\n Domain Extents:\\\\n   x-coordinate: min (m) = 0.000000e+00, max (m) = 2.000000e-01\\\\n   y-coordinate: min (m) = 0.000000e+00, max (m) = 2.000000e-02\\\\n Volume statistics:\\\\n   minimum volume (m3): 2.695799e-07\\\\n   maximum volume (m3): 5.611842e-07\\\\n     total volume (m3): 4.000000e-03\\\\n Face area statistics:\\\\n\\n…中间日志已省略，完整日志保存在任务目录…\\n       9258 cells,     1 zone  ...\\\\n       14107 faces,     4 zones ...\\\\n        4850 nodes,     1 zone  ...\\\\n  Done.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-130707-27e2af\\\\\\\\channel_velocity_repair_final.dat.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\n  Writing results.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-130707-27e2af\\\\\\\\post-130923-6f2c\\\\\\\\result.cas.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\nGrouping cells for Laplace smoothing ...\\\\n        9258 cells,     1 zone  ...\\\\n       14107 faces,     4 zones ...\\\\n        4850 nodes,     1 zone  ...\\\\n  Done.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-130707-27e2af\\\\\\\\post-130923-6f2c\\\\\\\\result.dat.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\n  Writing results.\\\\nDone.\\\\nCreating zone surface for fluid zone\\\\nEXPORT_RESULTS {'status': 'ok', 'directory': 'C:\\\\\\\\\\\\\\\\Users\\\\\\\\\\\\\\\\13977\\\\\\\\\\\\\\\\AppData\\\\\\\\\\\\\\\\Local\\\\\\\\\\\\\\\\FluentAGI\\\\\\\\\\\\\\\\data\\\\\\\\\\\\\\\\runs\\\\\\\\\\\\\\\\20261018-130707-27e2af\\\\\\\\\\\\\\\\post-130923-6f2c', 'created': '2026-10-18T13:09:23.686944', 'files': ['mesh.png', 'pressure.png', 'residual.csv', 'result.cas.h5', 'result.dat.h5', 'velocity-magnitude.png'], 'errors': [], 'convergence_verified': False}\\\\n实际残差和收敛提示记录在 channel_velocity_repair.trn；请结合各批日志判断收敛，导出文件以适配器实际返回结果为准。\\\\n\\\\nTranscript closed.\\\\n\\\", \\\"stderr\\\": \\\"\\\", \\\"return_value\\\": null, \\\"message\\\": null, \\\"error_code\\\": null, \\\"warnings\\\": []}\"}, {\"assistant\": \"本次已完成计算与保存，无需重复运行。\\n\\n网格：9258 个三角形单元，4850 个节点。\\n最终第 36 次迭代，Fluent 明确提示“solution is converged”，达到当前设置的残差判据。\\n最终残差：连续性 3.4656×10⁻⁴，x 速度 3.9597×10⁻⁶，y 速度 1.5044×10⁻⁷。\\n已保存最终 case/data：channel_velocity_repair_final.cas.h5、channel_velocity_repair_final.dat.h5。\\n后处理目录 post-130923-6f2c 已导出网格图、压力图、速度图和 residual.csv，返回错误列表为空。\\n\\n上述证据说明当前残差判据已满足；质量守恒误差和网格无关性尚未验证。\", \"run_directory\": \"C:\\\\Users\\\\13977\\\\AppData\\\\Local\\\\FluentAGI\\\\data\\\\runs\\\\20261018-130707-27e2af\"}, {\"user\": \"翼型绕流，也来一个，要求智能加密网格，自己定义，要求速度算快点，我现在在演示\"}, {\"tool\": \"run_code\", \"result\": \"{\\\"status\\\": \\\"ok\\\", \\\"stdout\\\": \\\"\\\\nOpening input/output transcript to file \\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\airfoil_repair.trn\\\\\\\".\\\\nCURRENT_MODELS {'multiphase': {'models': 'none', 'number_of_phases': 0}, 'energy': {'enabled': False}, 'viscous': {'model': 'laminar', 'options': {}}, 'radiation': {'model': 'none', 'solar_load': {'sun_direction_vector_definition': {}}}, 'species': {'model': {'option': 'off', 'number_vol_spec': False}}, 'discrete_pha\\n…中间日志已省略，完整日志保存在任务目录…\\n      9808 cells,     1 zone  ...\\\\n       14904 faces,     4 zones ...\\\\n        5096 nodes,     1 zone  ...\\\\n  Done.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\airfoil_repair_final.dat.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\n  Writing results.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\post-131337-8a52\\\\\\\\result.cas.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\nGrouping cells for Laplace smoothing ...\\\\n        9808 cells,     1 zone  ...\\\\n       14904 faces,     4 zones ...\\\\n        5096 nodes,     1 zone  ...\\\\n  Done.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\post-131337-8a52\\\\\\\\result.dat.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\n  Writing results.\\\\nDone.\\\\nCreating zone surface for fluid zone\\\\nEXPORT_RESULTS {'status': 'ok', 'directory': 'C:\\\\\\\\\\\\\\\\Users\\\\\\\\\\\\\\\\13977\\\\\\\\\\\\\\\\AppData\\\\\\\\\\\\\\\\Local\\\\\\\\\\\\\\\\FluentAGI\\\\\\\\\\\\\\\\data\\\\\\\\\\\\\\\\runs\\\\\\\\\\\\\\\\20261018-131135-2f3559\\\\\\\\\\\\\\\\post-131337-8a52', 'created': '2026-10-18T13:13:37.382274', 'files': ['mesh.png', 'pressure.png', 'residual.csv', 'result.cas.h5', 'result.dat.h5', 'velocity-magnitude.png'], 'errors': [], 'convergence_verified': False}\\\\n低雷诺数零攻角风洞演示；翼面距离场和尾迹区域预设加密。收敛依据 airfoil_repair.trn 中实际残差和收敛提示判断，导出成功与否依据 EXPORT_RESULTS 返回状态及错误列表判断。\\\\n\\\\n\\\", \\\"stderr\\\": \\\"\\\", \\\"return_value\\\": null, \\\"message\\\": null, \\\"error_code\\\": null, \\\"warnings\\\": []}\"}]\nRuntime capabilities:\n{\"protocol\": \"FluentAGI-capabilities-v1\", \"session\": {\"connected\": true, \"mode\": \"launch\"}, \"geometry\": {\"worker\": \"gmsh isolated process\", \"imports\": [], \"builtins\": [\"range\", \"len\", \"int\", \"float\", \"str\", \"list\", \"tuple\", \"enumerate\", \"zip\", \"min\", \"max\", \"abs\", \"round\", \"RuntimeError\", \"ValueError\", \"print\", \"set\", \"sum\", \"sorted\", \"bool\", \"all\", \"any\"], \"physical_groups\": [\"inlet\", \"outlet\", \"walls\"], \"cell_types\": [\"triangle\", \"quadrilateral\", \"tetrahedron\", \"hexahedron\", \"prism\", \"pyramid\"]}, \"script\": {\"imports\": [\"math\", \"json\", \"itertools\", \"functools\", \"collections\", \"dataclasses\", \"typing\"], \"adapters\": [\"build_dust_box\", \"configure_transient_dust\", \"initialize_transient_dust\", \"read_transient_dust\", \"advance_transient_dust\", \"resume_transient_dust\", \"read_transient_dust_results\", \"inspect_dpm\", \"configure_dpm\", \"create_dust_injection\", \"set_particle_boundaries\", \"track_particles\", \"build_planar\", \"build_volume\", \"build_extruded\", \"geometry_mesh\", \"configure_water_air\", \"initialize_air\", \"record_animation\", \"export_results\", \"assign_phase_materials\", \"assign_multiphase_materials\", \"configure_three_phase_materials\", \"audit_multiphase_interfaces\", \"configure_evaporation_condensation\", \"inspect_phase_change\", \"configure_surface_tension\", \"inspect_surface_tension\"]}, \"generated_at\": 1792300295.565992, \"phase_change\": {\"version\": \"v242\", \"model\": \"Lee\", \"adapter_multiphase_models\": [\"vof\"], \"mixture_officially_available\": true, \"mixture_adapter_validated\": false, \"two_phase_2d_correction_runtime_validation\": \"pending\", \"automatic_model_switch\": false, \"phases\": [2, 3], \"saturation\": \"constant K\", \"frequencies\": \"positive finite 1/s\", \"mass_transfer_pairs\": 1, \"internal_official_tui\": true, \"generated_direct_tui\": false, \"readback\": \"unique case snapshot\", \"initializes\": false}, \"surface_tension\": {\"version\": \"v242/v252\", \"runtime_validation\": {\"v242\": \"previous native validation\", \"v252\": \"official command and generated SDK checked; customer runtime readback required\"}, \"model\": \"VOF\", \"coefficient\": \"nonnegative finite N/m\", \"preserves_other_pairs\": true, \"readback\": \"unique case snapshot\", \"initializes\": false}, \"transient_dpm\": {\"version\": \"v242\", \"model\": \"unsteady single-phase carrier + transient one-way inert DPM\", \"release\": \"one short native pulse per explicit point / region grid, max 64 weighted parcels\", \"chunk_steps\": 60, \"positions\": \"native current positions at actual physical time; never steady replay\", \"checkpoint\": \"unique Case/Data plus SHA256 and particle-state readback\", \"acceptance\": \"each-step residuals, native air mass flux, particle mass/count fate closure\", \"default_residual_tolerance\": 1e-05, \"benchmark_residual_tolerance\": 0.001, \"strict_1e_5_initial_step_validated\": false, \"resuspension_validated\": false, \"stochastic_turbulent_dispersion_validated\": false}, \"dpm\": {\"version\": \"v242\", \"carrier\": \"single phase, one-way, steady inert dust\", \"injection_types\": [\"single\", \"group\"], \"surface_injection_validated\": false, \"boundary_types\": [\"reflect\", \"trap\", \"escape\"], \"trajectory_source\": \"native GetParticleTracksField RPC\", \"animation\": \"steady DPM trajectory residence-time replay, no carrier advance\", \"transient_dpm_validated\": false, \"two_way_validated\": false, \"readback\": true, \"active\": true}, \"fluent_version\": \"Ansys Fluent 2024 R2\", \"model_active\": true}\nCurrent session:\n{\"connected\": true, \"dimension\": 2, \"mode\": \"solver\", \"owned\": true, \"continuation\": true}\nTask directory:\nC:\\Users\\13977\\AppData\\Local\\FluentAGI\\data\\runs\\20261018-131135-2f3559\nCurrent request:\n翼型绕流，也来一个，要求智能加密网格，自己定义，要求速度算快点，我现在在演示\nDesktop execution feedback:\n[{\"failed_action\": {\"tool\": \"run_code\", \"arguments\": {\"code\": \"# Use the existing connected PyFluent variable solver.\\ntask_directory = r\\\"C:\\\\Users\\\\13977\\\\AppData\\\\Local\\\\FluentAGI\\\\data\\\\runs\\\\20261018-131135-2f3559\\\"\\nsettings = solver.settings\\ntranscript_started = False\\n\\ngmsh_code = \\\"\\\"\\\"\\ngmsh.model.add(\\\"naca0012_fast_demo\\\")\\nocc = gmsh.model.occ\\nchord = 0.1\\nn = 36\\nupper = []\\nlower = []\\nfor i in range(n + 1):\\n    x = 0.5 * (1.0 - math.cos(math.pi * i / n))\\n    yt = 5.0 * 0.12 * (\\n        0.2969 * math.sqrt(x)\\n        - 0.1260 * x\\n        - 0.3516 * x * x\\n        + 0.2843 * x * x * x\\n        - 0.1036 * x * x * x * x\\n    )\\n    if i == 0 or i == n:\\n        p = occ.addPoint(chord * x, 0.0, 0.0)\\n        upper.append(p)\\n        lower.append(p)\\n    else:\\n        upper.append(occ.addPoint(chord * x, chord * yt, 0.0))\\n        lower.append(occ.addPoint(chord * x, -chord * yt, 0.0))\\n\\ncu = occ.addSpline(upper)\\ncl = occ.addSpline(list(reversed(lower)))\\nfoil_loop = occ.addCurveLoop([cu, cl])\\np0 = occ.addPoint(-0.3, -0.3, 0)\\np1 = occ.addPoint(0.7, -0.3, 0)\\np2 = occ.addPoint(0.7, 0.3, 0)\\np3 = occ.addPoint(-0.3, 0.3, 0)\\nbottom = occ.addLine(p0, p1)\\nright = occ.addLine(p1, p2)\\ntop = occ.addLine(p2, p3)\\nleft = occ.addLine(p3, p0)\\nouter_loop = occ.addCurveLoop([bottom, right, top, left])\\nfluid = occ.addPlaneSurface([outer_loop, foil_loop])\\nocc.synchronize()\\n\\nfor name, curves in [\\n    (\\\"inlet\\\", [left]),\\n    (\\\"outlet\\\", [right]),\\n    (\\\"walls\\\", [bottom, top, cu, cl]),\\n]:\\n    tag = gmsh.model.addPhysicalGroup(1, curves)\\n    gmsh.model.setPhysicalName(1, tag, name)\\ntag = gmsh.model.addPhysicalGroup(2, [fluid])\\ngmsh.model.setPhysicalName(2, tag, \\\"fluid\\\")\\n\\ndistance = gmsh.model.mesh.field.add(\\\"Distance\\\")\\ngmsh.model.mesh.field.setNumbers(distance, \\\"CurvesList\\\", [cu, cl])\\ngmsh.model.mesh.field.setNumber(distance, \\\"Sampling\\\", 160)\\nnear = gmsh.model.mesh.field.add(\\\"Threshold\\\")\\ngmsh.model.mesh.field.setNumber(near, \\\"InField\\\", distance)\\ngmsh.model.mesh.field.setNumber(near, \\\"SizeMin\\\", 0.0008)\\ngmsh.model.mesh.field.setNumber(near, \\\"SizeMax\\\", 0.025)\\ngmsh.model.mesh.field.setNumber(near, \\\"DistMin\\\", 0.003)\\ngmsh.model.mesh.field.setNumber(near, \\\"DistMax\\\", 0.08)\\n\\nwake = gmsh.model.mesh.field.add(\\\"Box\\\")\\nfor key, value in [\\n    (\\\"VIn\\\", 0.004), (\\\"VOut\\\", 0.025),\\n    (\\\"XMin\\\", 0.085), (\\\"XMax\\\", 0.4),\\n    (\\\"YMin\\\", -0.025), (\\\"YMax\\\", 0.025),\\n    (\\\"ZMin\\\", -0.001), (\\\"ZMax\\\", 0.001),\\n    (\\\"Thickness\\\", 0.025),\\n]:\\n    gmsh.model.mesh.field.setNumber(wake, key, value)\\ncombined = gmsh.model.mesh.field.add(\\\"Min\\\")\\ngmsh.model.mesh.field.setNumbers(combined, \\\"FieldsList\\\", [near, wake])\\ngmsh.model.mesh.field.setAsBackgroundMesh(combined)\\ngmsh.option.setNumber(\\\"Mesh.MeshSizeFromPoints\\\", 0)\\ngmsh.option.setNumber(\\\"Mesh.MeshSizeFromCurvature\\\", 0)\\ngmsh.option.setNumber(\\\"Mesh.MeshSizeExtendFromBoundary\\\", 0)\\ngmsh.option.setNumber(\\\"Mesh.MeshSizeMin\\\", 0.0006)\\ngmsh.option.setNumber(\\\"Mesh.MeshSizeMax\\\", 0.025)\\ngmsh.option.setNumber(\\\"Mesh.ElementOrder\\\", 1)\\ngmsh.option.setNumber(\\\"Mesh.Algorithm\\\", 6)\\ngmsh.write(output_dir + \\\"/naca0012.step\\\")\\ngmsh.model.mesh.generate(2)\\ngmsh.model.mesh.optimize(\\\"Relocate2D\\\")\\n\\\"\\\"\\\"\\n\\ntry:\\n    settings.file.start_transcript(\\n        file_name=task_directory + r\\\"\\\\airfoil_demo.trn\\\"\\n    )\\n    transcript_started = True\\n\\n    if settings.setup.models.is_active():\\n        settings.file.write_case_data(\\n            file_name=task_directory + r\\\"\\\\previous_channel_backup.cas.h5\\\"\\n        )\\n\\n    mesh = fluentagi.geometry_mesh(\\n        directory=task_directory,\\n        code=gmsh_code,\\n    )\\n    print(\\\"AIRFOIL_MESH\\\", mesh)\\n    settings.file.read_mesh(file_name=mesh[\\\"mesh_file\\\"])\\n    settings.mesh.check()\\n\\n    if not settings.setup.models.is_active():\\n        raise RuntimeError(\\\"翼型网格读取后模型未激活。\\\")\\n\\n    settings.setup.general.solver.type = \\\"pressure-based\\\"\\n    settings.setup.general.solver.time = \\\"steady\\\"\\n    settings.setup.models.viscous.model = \\\"laminar\\\"\\n    settings.setup.models.energy.enabled = False\\n    settings.setup.general.operating_conditions.gravity.enable = False\\n\\n    air = settings.setup.materials.fluid[\\\"air\\\"]\\n    air.density.set_state({\\\"option\\\": \\\"constant\\\", \\\"value\\\": 1.225})\\n    air.viscosity.set_state({\\\"option\\\": \\\"constant\\\", \\\"value\\\": 1.7894e-5})\\n    print(\\\"AIR\\\", air.get_state())\\n    print(\\\"DEMO_PARAMETERS\\\", {\\n        \\\"airfoil\\\": \\\"NACA0012\\\",\\n        \\\"chord_m\\\": 0.1,\\n        \\\"velocity_m_s\\\": 0.1,\\n        \\\"angle_deg\\\": 0.0,\\n        \\\"Re_chord\\\": 1.225 * 0.1 * 0.1 / 1.7894e-5,\\n        \\\"model\\\": \\\"steady laminar\\\",\\n        \\\"refinement\\\": \\\"prescribed distance and wake fields\\\",\\n    })\\n\\n    zones = settings.setup.cell_zone_conditions.fluid\\n    for name in zones.get_object_names():\\n        zones[name].general.material = \\\"air\\\"\\n\\n    boundaries = settings.setup.boundary_conditions\\n    inlet = boundaries.velocity_inlet[\\\"inlet\\\"]\\n    inlet.momentum.velocity_specification_method = \\\"Magnitude, Normal to Boundary\\\"\\n    inlet.momentum.velocity.set_state({\\\"option\\\": \\\"value\\\", \\\"value\\\": 0.1})\\n    outlet = boundaries.pressure_outlet[\\\"outlet\\\"]\\n    outlet.momentum.gauge_pressure.set_state(\\n        {\\\"option\\\": \\\"value\\\", \\\"value\\\": 0.0}\\n    )\\n    for name in boundaries.wall.get_object_names():\\n        wall = boundaries.wall[name]\\n        wall.momentum.wall_motion = \\\"Stationary Wall\\\"\\n        wall.momentum.shear_condition = \\\"No Slip\\\"\\n\\n    print(\\\"INLET\\\", inlet.get_state())\\n    print(\\\"OUTLET\\\", outlet.get_state())\\n    print(\\\"WALLS\\\", boundaries.wall.get_state())\\n    print(\\\"RESIDUAL_SETTINGS\\\", settings.solution.monitor.residual.get_state())\\n\\n    settings.file.write_case(\\n        file_name=task_directory + r\\\"\\\\airfoil_configured.cas.h5\\\"\\n    )\\n    settings.solution.initialization.hybrid_initialize()\\n\\n    for batch in range(1, 4):\\n        print(\\\"BATCH_BEGIN\\\", batch, \\\"MAX_ITERATIONS\\\", 100)\\n        settings.solution.run_calculation.iterate(iter_count=100)\\n        print(\\\"BATCH_END\\\", batch)\\n        settings.file.write_case_data(\\n            file_name=task_directory\\n            + r\\\"\\\\airfoil_batch_\\\"\\n            + str(batch)\\n            + \\\".cas.h5\\\"\\n        )\\n\\n    settings.file.write_case_data(\\n        file_name=task_directory + r\\\"\\\\airfoil_final.cas.h5\\\"\\n    )\\n    result = fluentagi.export_results(\\n        directory=task_directory,\\n        fields=[\\\"pressure\\\", \\\"velocity-magnitude\\\"],\\n    )\\n    print(\\\"EXPORT_RESULTS\\\", result)\\n    print(\\n        \\\"本案例为低雷诺数零攻角风洞演示，采用预设空间局部加密，\\\"\\n        \\\"不是基于求解误差的自适应网格。\\\"\\n        \\\"实际收敛需核对 airfoil_demo.trn 和导出的 residual.csv；\\\"\\n        \\\"若未达到判据，保留当前解继续迭代，不重新初始化。\\\"\\n    )\\n\\nfinally:\\n    if transcript_started:\\n        settings.file.stop_transcript()\"}}, \"error\": \"{\\\"status\\\": \\\"error\\\", \\\"stdout\\\": \\\"\\\\nOpening input/output transcript to file \\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\airfoil_demo.trn\\\\\\\".\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\previous_channel_backup.cas.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\nGrouping cells for Laplace smoothing ...\\\\n        9258 cells,     1 zone  ...\\\\n       14107 faces,     4 zones ...\\\\n        4850 nodes,     1 zone  ...\\\\n  Done.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\previous_channel_backup.dat.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\n  Writing results.\\\\nDone.\\\\n\\\\n\\\", \\\"stderr\\\": \\\"\\\\nTraceback (most recent call last):\\\\n  File \\\\\\\"ansys\\\\\\\\fluent\\\\\\\\mcp\\\\\\\\solve\\\\\\\\backends\\\\\\\\pyfluent.py\\\\\\\", line 2793, in _do\\\\n    exec(  # noqa: S102  # nosec B102\\\\n  File \\\\\\\"<mcp>\\\\\\\", line 100, in <module>\\\\n  File \\\\\\\"automation.py\\\\\\\", line 84, in geometry_mesh\\\\n  File \\\\\\\"geometry.py\\\\\\\", line 21, in run_geometry\\\\n  File \\\\\\\"geometry.py\\\\\\\", line 15, in validate_geometry\\\\nValueError: 不允许的名称：reversed\\\\n\\\", \\\"return_value\\\": null, \\\"message\\\": \\\"不允许的名称：reversed\\\", \\\"error_code\\\": \\\"execution_error\\\", \\\"warnings\\\": []}\", \"note\": \"可能有部分操作已生效，请先检查实时状态，修复后继续。\"}, {\"action\": {\"tool\": \"run_code\", \"arguments\": {\"code\": \"# Use the existing connected PyFluent variable solver.\\ntask_directory = r\\\"C:\\\\Users\\\\13977\\\\AppData\\\\Local\\\\FluentAGI\\\\data\\\\runs\\\\20261018-131135-2f3559\\\"\\nsettings = solver.settings\\ntranscript_started = False\\n\\ngmsh_code = \\\"\\\"\\\"\\ngmsh.model.add(\\\"naca0012_fast_repair\\\")\\nocc = gmsh.model.occ\\nchord = 0.1\\nn = 36\\nupper = []\\nlower = []\\nfor i in range(n + 1):\\n    x = 0.5 * (1.0 - math.cos(math.pi * i / n))\\n    yt = 0.6 * (\\n        0.2969 * math.sqrt(x)\\n        - 0.1260 * x\\n        - 0.3516 * x * x\\n        + 0.2843 * x * x * x\\n        - 0.1036 * x * x * x * x\\n    )\\n    if i == 0 or i == n:\\n        p = occ.addPoint(chord * x, 0.0, 0.0)\\n        upper.append(p)\\n        lower.append(p)\\n    else:\\n        upper.append(occ.addPoint(chord * x, chord * yt, 0.0))\\n        lower.append(occ.addPoint(chord * x, -chord * yt, 0.0))\\ncu = occ.addSpline(upper)\\ncl = occ.addSpline(lower[::-1])\\nfoil_loop = occ.addCurveLoop([cu, cl])\\n\\np0 = occ.addPoint(-0.3, -0.3, 0)\\np1 = occ.addPoint(0.7, -0.3, 0)\\np2 = occ.addPoint(0.7, 0.3, 0)\\np3 = occ.addPoint(-0.3, 0.3, 0)\\nbottom = occ.addLine(p0, p1)\\nright = occ.addLine(p1, p2)\\ntop = occ.addLine(p2, p3)\\nleft = occ.addLine(p3, p0)\\nouter_loop = occ.addCurveLoop([bottom, right, top, left])\\nfluid = occ.addPlaneSurface([outer_loop, foil_loop])\\nocc.synchronize()\\n\\nfor name, curves in [\\n    (\\\"inlet\\\", [left]),\\n    (\\\"outlet\\\", [right]),\\n    (\\\"walls\\\", [bottom, top, cu, cl]),\\n]:\\n    tag = gmsh.model.addPhysicalGroup(1, curves)\\n    gmsh.model.setPhysicalName(1, tag, name)\\ntag = gmsh.model.addPhysicalGroup(2, [fluid])\\ngmsh.model.setPhysicalName(2, tag, \\\"fluid\\\")\\n\\ndistance = gmsh.model.mesh.field.add(\\\"Distance\\\")\\ngmsh.model.mesh.field.setNumbers(distance, \\\"CurvesList\\\", [cu, cl])\\ngmsh.model.mesh.field.setNumber(distance, \\\"Sampling\\\", 160)\\nnear = gmsh.model.mesh.field.add(\\\"Threshold\\\")\\nfor key, value in [\\n    (\\\"InField\\\", distance),\\n    (\\\"SizeMin\\\", 0.0008),\\n    (\\\"SizeMax\\\", 0.025),\\n    (\\\"DistMin\\\", 0.003),\\n    (\\\"DistMax\\\", 0.08),\\n]:\\n    gmsh.model.mesh.field.setNumber(near, key, value)\\n\\nwake = gmsh.model.mesh.field.add(\\\"Box\\\")\\nfor key, value in [\\n    (\\\"VIn\\\", 0.004), (\\\"VOut\\\", 0.025),\\n    (\\\"XMin\\\", 0.085), (\\\"XMax\\\", 0.4),\\n    (\\\"YMin\\\", -0.025), (\\\"YMax\\\", 0.025),\\n    (\\\"ZMin\\\", -0.001), (\\\"ZMax\\\", 0.001),\\n    (\\\"Thickness\\\", 0.025),\\n]:\\n    gmsh.model.mesh.field.setNumber(wake, key, value)\\ncombined = gmsh.model.mesh.field.add(\\\"Min\\\")\\ngmsh.model.mesh.field.setNumbers(combined, \\\"FieldsList\\\", [near, wake])\\ngmsh.model.mesh.field.setAsBackgroundMesh(combined)\\n\\nfor key, value in [\\n    (\\\"Mesh.MeshSizeFromPoints\\\", 0),\\n    (\\\"Mesh.MeshSizeFromCurvature\\\", 0),\\n    (\\\"Mesh.MeshSizeExtendFromBoundary\\\", 0),\\n    (\\\"Mesh.MeshSizeMin\\\", 0.0006),\\n    (\\\"Mesh.MeshSizeMax\\\", 0.025),\\n    (\\\"Mesh.ElementOrder\\\", 1),\\n    (\\\"Mesh.Algorithm\\\", 6),\\n]:\\n    gmsh.option.setNumber(key, value)\\ngmsh.write(output_dir + \\\"/naca0012.step\\\")\\ngmsh.model.mesh.generate(2)\\ngmsh.model.mesh.optimize(\\\"Relocate2D\\\")\\n\\\"\\\"\\\"\\n\\ntry:\\n    settings.file.start_transcript(\\n        file_name=task_directory + r\\\"\\\\airfoil_repair.trn\\\"\\n    )\\n    transcript_started = True\\n\\n    if settings.setup.models.is_active():\\n        print(\\\"CURRENT_MODELS\\\", settings.setup.models.get_state())\\n        settings.file.write_case_data(\\n            file_name=task_directory + r\\\"\\\\before_airfoil_repair.cas.h5\\\"\\n        )\\n\\n    mesh = fluentagi.geometry_mesh(\\n        directory=task_directory,\\n        code=gmsh_code,\\n    )\\n    print(\\\"AIRFOIL_MESH\\\", mesh)\\n    settings.file.read_mesh(file_name=mesh[\\\"mesh_file\\\"])\\n    settings.mesh.check()\\n\\n    if not settings.setup.models.is_active():\\n        raise RuntimeError(\\\"翼型网格读入后模型未激活。\\\")\\n\\n    settings.setup.general.solver.type = \\\"pressure-based\\\"\\n    settings.setup.general.solver.time = \\\"steady\\\"\\n    settings.setup.models.viscous.model = \\\"laminar\\\"\\n    settings.setup.models.energy.enabled = False\\n    settings.setup.general.operating_conditions.gravity.enable = False\\n\\n    air = settings.setup.materials.fluid[\\\"air\\\"]\\n    air.density.set_state({\\\"option\\\": \\\"constant\\\", \\\"value\\\": 1.225})\\n    air.viscosity.set_state({\\\"option\\\": \\\"constant\\\", \\\"value\\\": 1.7894e-5})\\n    print(\\\"AIR_READBACK\\\", air.get_state())\\n\\n    zones = settings.setup.cell_zone_conditions.fluid\\n    zone_names = zones.get_object_names()\\n    if not zone_names:\\n        raise RuntimeError(\\\"没有流体单元区。\\\")\\n    for name in zone_names:\\n        zones[name].general.material = \\\"air\\\"\\n\\n    boundaries = settings.setup.boundary_conditions\\n    inlet = boundaries.velocity_inlet[\\\"inlet\\\"]\\n    inlet.momentum.velocity_specification_method = \\\"Magnitude, Normal to Boundary\\\"\\n    inlet.momentum.velocity.set_state({\\\"option\\\": \\\"value\\\", \\\"value\\\": 0.1})\\n    outlet = boundaries.pressure_outlet[\\\"outlet\\\"]\\n    outlet.momentum.gauge_pressure.set_state(\\n        {\\\"option\\\": \\\"value\\\", \\\"value\\\": 0.0}\\n    )\\n    for name in boundaries.wall.get_object_names():\\n        wall = boundaries.wall[name]\\n        wall.momentum.wall_motion = \\\"Stationary Wall\\\"\\n        wall.momentum.shear_condition = \\\"No Slip\\\"\\n        print(\\\"WALL_READBACK\\\", name, wall.get_state())\\n\\n    velocity_state = inlet.momentum.velocity.get_state()\\n    pressure_state = outlet.momentum.gauge_pressure.get_state()\\n    print(\\\"INLET_READBACK\\\", velocity_state)\\n    print(\\\"OUTLET_READBACK\\\", pressure_state)\\n    if abs(velocity_state[\\\"value\\\"] - 0.1) > 1e-10:\\n        raise RuntimeError(\\\"入口速度读回不符。\\\")\\n    if abs(pressure_state[\\\"value\\\"]) > 1e-10:\\n        raise RuntimeError(\\\"出口表压读回不符。\\\")\\n\\n    print(\\\"RE_CHORD\\\", 1.225 * 0.1 * 0.1 / 1.7894e-5)\\n    print(\\\"RESIDUAL_SETTINGS\\\", settings.solution.monitor.residual.get_state())\\n    settings.file.write_case(\\n        file_name=task_directory + r\\\"\\\\airfoil_repair_configured.cas.h5\\\"\\n    )\\n    settings.solution.initialization.hybrid_initialize()\\n\\n    for batch in range(1, 4):\\n        print(\\\"BATCH_BEGIN\\\", batch, \\\"MAX_ITERATIONS\\\", 100)\\n        settings.solution.run_calculation.iterate(iter_count=100)\\n        print(\\\"BATCH_END\\\", batch)\\n        settings.file.write_case_data(\\n            file_name=task_directory\\n            + r\\\"\\\\airfoil_repair_batch_\\\"\\n            + str(batch)\\n            + \\\".cas.h5\\\"\\n        )\\n\\n    settings.file.write_case_data(\\n        file_name=task_directory + r\\\"\\\\airfoil_repair_final.cas.h5\\\"\\n    )\\n    result = fluentagi.export_results(\\n        directory=task_directory,\\n        fields=[\\\"pressure\\\", \\\"velocity-magnitude\\\"],\\n    )\\n    print(\\\"EXPORT_RESULTS\\\", result)\\n    print(\\n        \\\"低雷诺数零攻角风洞演示；翼面距离场和尾迹区域预设加密。\\\"\\n        \\\"收敛依据 airfoil_repair.trn 中实际残差和收敛提示判断，\\\"\\n        \\\"导出成功与否依据 EXPORT_RESULTS 返回状态及错误列表判断。\\\"\\n    )\\n\\nfinally:\\n    if transcript_started:\\n        settings.file.stop_transcript()\"}}, \"result\": \"{\\\"status\\\": \\\"ok\\\", \\\"stdout\\\": \\\"\\\\nOpening input/output transcript to file \\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\airfoil_repair.trn\\\\\\\".\\\\nCURRENT_MODELS {'multiphase': {'models': 'none', 'number_of_phases': 0}, 'energy': {'enabled': False}, 'viscous': {'model': 'laminar', 'options': {}}, 'radiation': {'model': 'none', 'solar_load': {'sun_direction_vector_definition': {}}}, 'species': {'model': {'option': 'off', 'number_vol_spec': False}}, 'discrete_phase': {'general_settings': {'interaction': {'enabled': False}, 'contour_plotting': 'none'}, 'physical_model\\n…中间日志已省略，完整日志保存在任务目录…\\n00:00   66\\\\n   135  1.1351e-03  1.2781e-06  1.5643e-07  0:00:00   65\\\\n   136  1.0721e-03  1.2193e-06  1.4467e-07  0:00:00   64\\\\n   137  1.0233e-03  1.1662e-06  1.3635e-07  0:00:00   63\\\\n   138  9.8291e-04  1.1212e-06  1.3217e-07  0:00:00   62\\\\n!  138 solution is converged\\\\nBATCH_END 2\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\airfoil_repair_batch_2.cas.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\nGrouping cells for Laplace smoothing ...\\\\n        9808 cells,     1 zone  ...\\\\n       14904 faces,     4 zones ...\\\\n        5096 nodes,     1 zone  ...\\\\n  Done.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\airfoil_repair_batch_2.dat.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\n  Writing results.\\\\nDone.\\\\nBATCH_BEGIN 3 MAX_ITERATIONS 100\\\\n\\\\n  iter  continuity  x-velocity  y-velocity     time/iter\\\\n   138  9.8291e-04  1.1212e-06  1.3217e-07  0:00:00  100\\\\n!  138 solution is converged\\\\n   139  9.3792e-04  1.0905e-06  1.2808e-07  0:00:00   99\\\\n!  139 solution is converged\\\\nBATCH_END 3\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\airfoil_repair_batch_3.cas.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\nGrouping cells for Laplace smoothing ...\\\\n        9808 cells,     1 zone  ...\\\\n       14904 faces,     4 zones ...\\\\n        5096 nodes,     1 zone  ...\\\\n  Done.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\airfoil_repair_batch_3.dat.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\n  Writing results.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\airfoil_repair_final.cas.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\nGrouping cells for Laplace smoothing ...\\\\n        9808 cells,     1 zone  ...\\\\n       14904 faces,     4 zones ...\\\\n        5096 nodes,     1 zone  ...\\\\n  Done.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\airfoil_repair_final.dat.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\n  Writing results.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\post-131337-8a52\\\\\\\\result.cas.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\nGrouping cells for Laplace smoothing ...\\\\n        9808 cells,     1 zone  ...\\\\n       14904 faces,     4 zones ...\\\\n        5096 nodes,     1 zone  ...\\\\n  Done.\\\\nDone.\\\\n\\\\nWriting to Austra:\\\\\\\"C:\\\\\\\\Users\\\\\\\\13977\\\\\\\\AppData\\\\\\\\Local\\\\\\\\FluentAGI\\\\\\\\data\\\\\\\\runs\\\\\\\\20261018-131135-2f3559\\\\\\\\post-131337-8a52\\\\\\\\result.dat.h5\\\\\\\" in NODE0 mode and compression level 1 ...\\\\n  Writing results.\\\\nDone.\\\\nCreating zone surface for fluid zone\\\\nEXPORT_RESULTS {'status': 'ok', 'directory': 'C:\\\\\\\\\\\\\\\\Users\\\\\\\\\\\\\\\\13977\\\\\\\\\\\\\\\\AppData\\\\\\\\\\\\\\\\Local\\\\\\\\\\\\\\\\FluentAGI\\\\\\\\\\\\\\\\data\\\\\\\\\\\\\\\\runs\\\\\\\\\\\\\\\\20261018-131135-2f3559\\\\\\\\\\\\\\\\post-131337-8a52', 'created': '2026-10-18T13:13:37.382274', 'files': ['mesh.png', 'pressure.png', 'residual.csv', 'result.cas.h5', 'result.dat.h5', 'velocity-magnitude.png'], 'errors': [], 'convergence_verified': False}\\\\n低雷诺数零攻角风洞演示；翼面距离场和尾迹区域预设加密。收敛依据 airfoil_repair.trn 中实际残差和收敛提示判断，导出成功与否依据 EXPORT_RESULTS 返回状态及错误列表判断。\\\\n\\\\n\\\", \\\"stderr\\\": \\\"\\\", \\\"return_value\\\": null, \\\"message\\\": null, \\\"error_code\\\": null, \\\"warnings\\\": []}\"}]",
      "reply": "ChatGPT 说：\n\n<final_answer>翼型绕流演示已完成，当前结果保留，无需重复运行。\n\nNACA0012，弦长 0.1 m、零攻角、空气速度 0.1 m/s。\n翼面和尾迹局部加密，实际网格 9808 个单元、5096 个节点。\n第 138 次迭代首次满足当前收敛判据，最终第 139 次仍提示收敛。\n最终残差：连续性 9.3792×10⁻⁴，x 速度 1.0905×10⁻⁶，y 速度 1.2808×10⁻⁷。\n已保存 airfoil_repair_final.cas.h5 和对应 dat.h5。\npost-131337-8a52 内已导出网格图、压力图、速度图及 residual.csv，导出无报错。\n\n这是低雷诺数层流演示；质量守恒和网格无关性尚未验证。</final_answer>",
      "executed_script": ""
    }
  ],
  "assessment": "翼型绕流演示已完成，当前结果保留，无需重复运行。\n\nNACA0012，弦长 0.1 m、零攻角、空气速度 0.1 m/s。\n翼面和尾迹局部加密，实际网格 9808 个单元、5096 个节点。\n第 138 次迭代首次满足当前收敛判据，最终第 139 次仍提示收敛。\n最终残差：连续性 9.3792×10⁻⁴，x 速度 1.0905×10⁻⁶，y 速度 1.2808×10⁻⁷。\n已保存 airfoil_repair_final.cas.h5 和对应 dat.h5。\npost-131337-8a52 内已导出网格图、压力图、速度图及 residual.csv，导出无报错。\n\n这是低雷诺数层流演示；质量守恒和网格无关性尚未验证。",
  "note": "仅包含此任务由 FluentAGI 发送和读取的聊天，非整个网页历史；执行脚本成功不代表物理收敛。"
}