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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

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npx -y skills add a5c-ai/babysitter --skill cfd-fluids

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SKILL.md

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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

  1. CAD Cleanup

    • Remove small features (< 3 cells)
    • Fill gaps and holes
    • Create smooth transitions
    • Define fluid domain boundaries
  2. Domain Definition

    • Internal flow: Extract fluid volume
    • External flow: Create far-field boundary
    • Symmetry: Identify planes of symmetry
    • Periodic: Define periodic pairs

Mesh Generation

  1. Mesh Types

    TypeApplicationPros/Cons
    Structured hexSimple geometriesHigh quality, more effort
    Unstructured tetComplex geometriesFlexible, more cells
    PolyhedralComplex internalGood quality, moderate count
    HybridMixed regionsOptimized for accuracy
  2. 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)
    
  3. 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

ModelApplicationWall Treatment
k-epsilon StandardGeneral industrialWall functions
k-epsilon RealizableRotation, separationWall functions
k-omega SSTAerospace, separationLow-Re or wall functions
Spalart-AllmarasExternal aeroLow-Re
LES/DESUnsteady, vortex sheddingWall-resolved

Boundary Conditions

  1. Inlet Conditions

    • Mass flow rate or velocity
    • Turbulence intensity (1-5% typical)
    • Hydraulic diameter or length scale
    • Temperature (if energy equation)
  2. Outlet Conditions

    • Pressure outlet (most common)
    • Outflow (fully developed)
    • Mass flow outlet (specified)
  3. Wall Conditions

    • No-slip (default)
    • Roughness (if significant)
    • Thermal (adiabatic, fixed T, heat flux)

Solution Settings

  1. Discretization Schemes

    Convection: Second-order upwind (accuracy)
                First-order (stability)
    Pressure: PRESTO (complex geometry)
              Standard (simple geometry)
    
  2. Convergence Criteria

    Residuals: < 1e-4 (typical)
               < 1e-6 (high accuracy)
    
    Monitor: Mass imbalance < 0.1%
             Force convergence
    

Post-Processing

  1. Flow Visualization

    • Streamlines and pathlines
    • Velocity vectors
    • Contour plots (P, V, T)
    • Surface integral reports
  2. 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

  1. Always perform mesh independence study
  2. Verify y+ values match turbulence model requirements
  3. Monitor mass and energy imbalance
  4. Validate with experimental data when available
  5. Start with steady-state before transient
  6. 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

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