--- name: cae description: Computer-aided engineering analysis license: MIT compatibility: opencode metadata: audience: engineers, analysts, designers category: engineering --- ## What I do - Perform finite element analysis (FEA) for structural analysis - Conduct computational fluid dynamics (CFD) simulations - Run thermal and heat transfer analyses - Perform modal analysis and vibration studies - Support optimization and topology optimization ## When to use me - When validating designs against physical loads - When analyzing stress and deformation in structures - When simulating fluid flow and heat transfer - When optimizing designs for weight or performance - When predicting product behavior before physical testing ## Key Concepts ### FEA Fundamentals ```python # Basic FEA workflow class FEAAnalysis: def __init__(self, geometry, mesh_params): self.geometry = geometry self.mesh_params = mesh_params self.boundary_conditions = [] self.loads = [] def mesh(self): """Generate finite element mesh""" return { "nodes": self._generate_nodes(), "elements": self._generate_elements(), "element_type": self.mesh_params.get("type", "tetrahedral") } def apply_boundary_conditions(self, bcs): """Apply displacement constraints""" self.boundary_conditions = bcs def apply_loads(self, loads): """Apply forces, pressures, temperatures""" self.loads = loads def solve(self): """Solve system of equations""" # K * u = F stiffness_matrix = self._assemble_stiffness() load_vector = self._assemble_loads() displacement = self._solve(stiffness_matrix, load_vector) return displacement def postprocess(self, results): """Calculate stresses, strains""" return { "displacement": results, "stress": self._compute_stress(results), "strain": self._compute_strain(results) } ``` ### Element Types | Element | DOFs | Applications | |---------|------|--------------| | Tetrahedron (3D) | 3/node | Complex 3D solids | | Hexahedron (3D) | 3/node | Structured meshes | | Triangle (2D) | 2/node | 2D plane stress/strain | | Quadrilateral (2D) | 2/node | 2D with bending | | Beam | 6/node | Structural frames | | Shell | 5-6/node | Thin structures | ### Analysis Types ```python # Static structural analysis STATIC_ANALYSIS = { "equation": "[K]{u} = {F}", "assumptions": "Linear, time-independent", "outputs": ["displacement", "stress", strain"] } # Modal analysis MODAL_ANALYSIS = { "equation": "[K]{phi} = omega^2 [M]{phi}", "purpose": "Natural frequencies, mode shapes", "outputs": ["frequencies", "mode_shapes"] } # Thermal analysis THERMAL_ANALYSIS = { "types": ["steady-state", "transient"], "equation": "[K]{T} = {Q}", "outputs": ["temperature", "heat_flux"] } ``` ### Mesh Quality Metrics | Metric | Good | Acceptable | Poor | |--------|------|------------|------| | Aspect ratio | < 3 | < 5 | > 10 | | Jacobian | > 0.5 | > 0.3 | < 0.1 | | Skewness | < 20° | < 40° | > 60° | | Warpage | < 5° | < 15° | > 30° | ### Common CAE Software | Software | Analysis Types | |----------|----------------| | ANSYS | Structural, Thermal, CFD, Multi-physics | | ABAQUS | Structural, Nonlinear, Dynamic | | COMSOL | Multi-physics coupling | | NASTRAN | Structural, Aeroelasticity | | STAR-CCM+ | CFD, Multi-physics | | Altair HyperWorks | Optimization, Structural |