Agent skill

fea-structural

Deep integration with finite element analysis tools for structural simulation across static, dynamic, and nonlinear domains

Stars 514
Forks 31

Install this agent skill to your Project

npx add-skill https://github.com/a5c-ai/babysitter/tree/main/library/specializations/domains/science/mechanical-engineering/skills/fea-structural

Metadata

Additional technical details for this skill

phase
1
domain
science
category
structural-analysis
priority
high
specialization
mechanical-engineering
tools libraries
[
    "ANSYS Mechanical",
    "Abaqus",
    "MSC NASTRAN",
    "HyperMesh",
    "Femap"
]

SKILL.md

Finite Element Analysis Skill

Purpose

The Finite Element Analysis skill provides deep integration with FEA tools for structural simulation, enabling systematic setup, execution, and post-processing of finite element models across static, dynamic, and nonlinear analysis domains.

Capabilities

  • ANSYS Mechanical, Abaqus, NASTRAN model setup and execution
  • Mesh generation strategies and quality assessment
  • Element type selection and convergence studies
  • Boundary condition specification and load case management
  • Linear and nonlinear static analysis configuration
  • Results post-processing and margin of safety calculation
  • Mesh independence and sensitivity studies
  • Report generation with stress/deflection contours

Usage Guidelines

Model Setup

Geometry Preparation

  1. CAD Import and Cleanup

    • Defeature small holes and fillets (analysis dependent)
    • Remove unnecessary detail
    • Verify watertight geometry
    • Create symmetry conditions if applicable
  2. Geometry Partitioning

    • Partition for mesh control
    • Create virtual topology for hex meshing
    • Identify contact surfaces
    • Define load application regions

Mesh Generation

  1. Element Selection

    Analysis Type Recommended Elements
    Static stress Hex20, Tet10, Quad8
    Thin structures Shell (QUAD4/8, TRIA3/6)
    Beam structures BEAM/BAR elements
    Contact Linear elements preferred
    Nonlinear Reduced integration with hourglass control
  2. Mesh Quality Criteria

    Aspect ratio: < 5 (< 3 preferred)
    Jacobian: > 0.6
    Warpage: < 15 degrees
    Skewness: < 0.8
    
  3. Mesh Refinement

    • Refine at stress concentrations
    • Transition ratios < 1.5
    • Multiple elements through thickness
    • Convergence study requirements

Analysis Configuration

Boundary Conditions

  1. Constraints

    • Fixed (all DOF constrained)
    • Pinned (translations fixed, rotations free)
    • Symmetry (appropriate DOF constrained)
    • Prescribed displacement
  2. Best Practices

    • Avoid over-constraint
    • Use RBE2/RBE3 for load distribution
    • Consider realistic support stiffness
    • Document all assumptions

Load Application

  1. Load Types

    • Pressure (uniform, hydrostatic)
    • Force (point, distributed)
    • Moment/torque
    • Thermal loads
    • Inertial loads (gravity, acceleration)
  2. Load Cases

    • Define all operational load cases
    • Include limit and ultimate factors
    • Combine per applicable standards
    • Document load derivation

Results Post-Processing

Stress Evaluation

  1. Stress Quantities

    • von Mises (ductile materials)
    • Principal stresses (fatigue, brittle)
    • Membrane + bending (shells)
    • Interlaminar (composites)
  2. Margin of Safety

    MS = (Allowable / Applied) - 1
    MS > 0 indicates positive margin
    
  3. Reporting

    • Maximum stress location and value
    • Stress contour plots
    • Deflection summary
    • Reaction forces verification

Process Integration

  • ME-006: Finite Element Analysis (FEA) Setup and Execution
  • ME-007: Stress and Deflection Analysis
  • ME-009: Nonlinear Structural Analysis

Input Schema

json
{
  "geometry": "CAD file path or description",
  "material": {
    "name": "string",
    "E": "number (Pa)",
    "nu": "number",
    "yield": "number (Pa)",
    "ultimate": "number (Pa)"
  },
  "loads": [
    {
      "type": "pressure|force|moment|thermal",
      "magnitude": "number",
      "location": "string",
      "direction": "array [x,y,z]"
    }
  ],
  "constraints": [
    {
      "type": "fixed|pinned|symmetry",
      "location": "string",
      "dof": "array"
    }
  ],
  "analysis_type": "static|modal|nonlinear",
  "output_requests": ["stress", "displacement", "reactions"]
}

Output Schema

json
{
  "analysis_results": {
    "max_stress": {
      "von_mises": "number (Pa)",
      "location": "string",
      "element_id": "number"
    },
    "max_displacement": {
      "magnitude": "number (m)",
      "location": "string",
      "node_id": "number"
    },
    "reaction_forces": {
      "total": "array [Fx, Fy, Fz, Mx, My, Mz]"
    }
  },
  "margin_of_safety": {
    "yield": "number",
    "ultimate": "number",
    "critical_location": "string"
  },
  "mesh_quality": {
    "element_count": "number",
    "worst_aspect_ratio": "number",
    "convergence_status": "string"
  }
}

Best Practices

  1. Always perform mesh convergence studies for critical analyses
  2. Verify reaction forces match applied loads
  3. Check for rigid body modes in modal analysis
  4. Use appropriate element formulations for contact
  5. Document all modeling assumptions and simplifications
  6. Compare results with hand calculations where possible

Integration Points

  • Connects with CAD Modeling for geometry import
  • Feeds into Fatigue Life Prediction for durability assessment
  • Supports Test Correlation for model validation
  • Integrates with Thermal Analysis for coupled problems

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