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Aircraft Modification – Structural Substantiation
Forward Side Skin Panel
Linear and nonlinear structural assessment of an equipment-rack side panel under emergency landing loads
Aircraft
DHC-8-100
Installation
Interior
Analysis
Linear Static FEA; Nonlinear Static FEA; Principal Stress; Plasticity; Fastener Pull-Out
Solver
Simcenter Nastran SOL 101; Simcenter Nastran SOL 106
Skills Demonstrated
FEM Idealization; Boundary Conditions; Load Distribution; Material Nonlinearity; Fastener Analysis; Margin of Safety
Engineering Tools
Simcenter Nastran; SolidWorks
Certification Basis
FAR 25.561
Project Category
Aircraft Modification – Structural Substantiation