CFD Analysis Skill
SkillDev toolsDeep integration with computational fluid dynamics tools for internal and external flow analysis
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Then ask your AI: use the CFD Analysis Skill skill
What this skill tells your AI
The instructions your AI receives, as published by a5c-ai/babysitter in library/specializations/domains/science/mechanical-engineering/skills/cfd-fluids/SKILL.md and read by ahel’s review.
Purpose
The CFD Analysis skill provides deep integration with computational fluid dynamics tools for internal and external flow analysis, enabling systematic setup, execution, and post-processing of fluid simulations.
Capabilities
- ANSYS Fluent, CFX, OpenFOAM workflow automation
- Mesh generation for complex geometries (structured, unstructured)
- Turbulence model selection (k-epsilon, k-omega, SST, LES)
- Boundary condition specification (inlet, outlet, wall, symmetry)
- Steady-state and transient flow simulations
- Post-processing for pressure, velocity, and flow visualization
- Mesh independence studies and validation
- Pressure drop and flow coefficient calculations
Usage Guidelines
Pre-Processing
Geometry Preparation
-
CAD Cleanup
- Remove small features (< 3 cells)
- Fill gaps and holes
- Create smooth transitions
- Define fluid domain boundaries
-
Domain Definition
- Internal flow: Extract fluid volume
- External flow: Create far-field boundary
- Symmetry: Identify planes of symmetry
- Periodic: Define periodic pairs
Mesh Generation
-
Mesh Types
Type Application Pros/Cons Structured hex Simple geometries High quality, more effort Unstructured tet Complex geometries Flexible, more cells Polyhedral Complex internal Good quality, moderate count Hybrid Mixed regions Optimized for accuracy -
Boundary Layer Mesh
First cell height: y+ = 1 (wall-resolved) y+ = 30-300 (wall functions) y = y+ * mu / (rho * u_tau) u_tau = sqrt(tau_w / rho) -
Mesh Quality Criteria
Orthogonality: > 0.1 (> 0.3 preferred) Skewness: < 0.95 (< 0.8 preferred) Aspect ratio: < 100 (< 20 near walls)
Solver Configuration
Turbulence Models
| Model | Application | Wall Treatment |
|---|---|---|
| k-epsilon Standard | General industrial | Wall functions |
| k-epsilon Realizable | Rotation, separation | Wall functions |
| k-omega SST | Aerospace, separation | Low-Re or wall functions |
| Spalart-Allmaras | External aero | Low-Re |
| LES/DES | Unsteady, vortex shedding | Wall-resolved |
Boundary Conditions
-
Inlet Conditions
- Mass flow rate or velocity
- Turbulence intensity (1-5% typical)
- Hydraulic diameter or length scale
- Temperature (if energy equation)
-
Outlet Conditions
- Pressure outlet (most common)
- Outflow (fully developed)
- Mass flow outlet (specified)
-
Wall Conditions
- No-slip (default)
- Roughness (if significant)
- Thermal (adiabatic, fixed T, heat flux)
Solution Settings
-
Discretization Schemes
Convection: Second-order upwind (accuracy) First-order (stability) Pressure: PRESTO (complex geometry) Standard (simple geometry) -
Convergence Criteria
Residuals: < 1e-4 (typical) < 1e-6 (high accuracy) Monitor: Mass imbalance < 0.1% Force convergence
Post-Processing
-
Flow Visualization
- Streamlines and pathlines
- Velocity vectors
- Contour plots (P, V, T)
- Surface integral reports
-
Quantitative Results
- Pressure drop
- Flow coefficient (Cv)
- Heat transfer coefficient
- Force and moment
Process Integration
- ME-010: Computational Fluid Dynamics (CFD) Analysis
Input Schema
{
"geometry": "CAD file path",
"flow_type": "internal|external",
"fluid": {
"name": "string",
"density": "number (kg/m3)",
"viscosity": "number (Pa.s)",
"specific_heat": "number (J/kg.K, if thermal)"
},
"inlet": {
"type": "velocity|mass_flow|pressure",
"value": "number",
"temperature": "number (K, if thermal)"
},
"outlet": {
"type": "pressure|outflow",
"value": "number (if pressure)"
},
"analysis_type": "steady|transient",
"turbulence_model": "k-epsilon|k-omega-sst|spalart-allmaras|laminar"
}
Output Schema
{
"flow_results": {
"pressure_drop": "number (Pa)",
"flow_coefficient": "number (Cv)",
"max_velocity": "number (m/s)",
"reynolds_number": "number"
},
"forces": {
"drag": "number (N)",
"lift": "number (N)",
"moment": "array [Mx, My, Mz]"
},
"thermal_results": {
"heat_transfer_rate": "number (W)",
"average_htc": "number (W/m2.K)",
"outlet_temperature": "number (K)"
},
"mesh_statistics": {
"cell_count": "number",
"y_plus_range": [min, max],
"orthogonality_min": "number"
},
"convergence": {
"iterations": "number",
"residuals": "object",
"mass_imbalance": "number"
}
}
Best Practices
- Always perform mesh independence study
- Verify y+ values match turbulence model requirements
- Monitor mass and energy imbalance
- Validate with experimental data when available
- Start with steady-state before transient
- Use appropriate turbulence model for flow physics
Integration Points
- Connects with CAD Modeling for geometry
- Feeds into Thermal Analysis for conjugate heat transfer
- Supports Heat Exchanger Design for performance prediction
- Integrates with Test Correlation for validation
Signals
- GitHub stars
- 2k
- Forks
- 112
- Last commit
- Sep 2026
Advanced
- Item type
- skill
- Key
cfd-fluids- Source
- github.com/a5c-ai/babysitter