Cfd fluids
Skill a5c-ai/babysitter/library/specializations/domains/science/mechanical-engineering/skills/cfd-fluids
Deep integration with computational fluid dynamics tools for internal and external flow analysisFrom its SKILL.md
npx -y skills add a5c-ai/babysitter --skill cfd-fluidsAssembled from the repository path, not quoted from the project. Check it against their README if it does not work.
SKILL.md
5.8 KB, ~1.4k tokens by cl100k_base, as published. Nobody here has run it
CFD Analysis Skill
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
What ships with it
Read from the repository
Just SKILL.md. No reference files, no scripts.