Babysitter cfd-fluids
Deep integration with computational fluid dynamics tools for internal and external flow analysis
install
source · Clone the upstream repo
git clone https://github.com/a5c-ai/babysitter
Claude Code · Install into ~/.claude/skills/
T=$(mktemp -d) && git clone --depth=1 https://github.com/a5c-ai/babysitter "$T" && mkdir -p ~/.claude/skills && cp -r "$T/library/specializations/domains/science/mechanical-engineering/skills/cfd-fluids" ~/.claude/skills/a5c-ai-babysitter-cfd-fluids && rm -rf "$T"
manifest:
library/specializations/domains/science/mechanical-engineering/skills/cfd-fluids/SKILL.mdsource content
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