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Aircraft Modification – Structural Substantiation
Radome Cooling System Installation
Static strength substantiation of external radome cooling components, composite attachments, and radome cutouts under aerodynamic loading
Aircraft
DHC-8-100
Installation
Exterior
Analysis
Classical Stress Analysis; Aerodynamic Loads; Rigid Body Analysis; Classical Laminate Theory; Composite Failure; Stress Concentration
Solver
N/A (Analytical)
Skills Demonstrated
Aerodynamic Load Estimation; Composite Analysis; Joint Allowables; Fastener Analysis; Stress Concentrations; Margin of Safety
Engineering Tools
Excel; 3D-RBA; Lamina Stress Analysis
Certification Basis
FAR Part 25; FAR 25.321–25.351
Project Category
Aircraft Modification – Structural Substantiation