A Collection of Technical Papers, Volume 2 |
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adhesive aerobraking aerodynamic aeroelastic Aeronautics and Astronautics AIAA aileron aircraft airplane alloy aluminum amplitude analysis analytical angle of attack applied Astronautics baseline bending bond buckling composite compressive concepts configuration constant crack growth rate crack length curve cycle damage tolerance damping displacement effect elastic energy Engineers equations evaluated experimental failure fatigue crack growth fibre finite element flaperon flaw flight Flight Dynamics flutter speed fracture mechanics fracture toughness frequency function fuselage inch incremental Institute of Aeronautics laminate linear load Lockheed-Georgia Company Mach number material matrix maximum method modal mode mode shapes nonlinear obtained optimality overload panels parameters peak plate predicted pressure problem ratio response shear shear strength shear stress shell shown in Figure Shuttle skin specimens spectrum stiffened stiffness strain strength stress intensity factor surface tensile theory thickness tion titanium transonic values weight welding wing