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Aircraft Modification – Structural Substantiation
Mission Radar Radome Installation
Static strength substantiation of an external mission radar radome, composite flange, and aircraft attachment system under aerodynamic loading
Aircraft
DHC-8-100
Installation
Exterior
Analysis
Aerodynamic Load Analysis; Rigid Body Analysis; Classical Laminate Theory; Composite Failure; Bearing & Pull-Through; Adhesive Shear
Solver
N/A (Analytical)
Skills Demonstrated
Aerodynamic Load Estimation; Composite Analysis; Load Path Assessment; Joint Allowables; Fastener Analysis; Margin of Safety
Engineering Tools
Excel; 3D-RBA; Lamina Stress Analysis
Certification Basis
FAR Part 25
Project Category
Aircraft Modification – Structural Substantiation