A Collection of Technical Papers: AIAA/ASME/ASCE/AHS 26th Structures, Structural Dynamics and Materials Conference, April 15-17, 1985, Orlando, Florida
American Institute of Aeronautics and Astronautics, American Society of Mechanical Engineers, Society of Automotive Engineers
American Institute of Aeronautics and Astronautics, 1975 - Science - 5 pages
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adhesive aerobraking aerodynamic aeroelastic Aeronautics and Astronautics AIAA aircraft airplane alloy aluminum American Institute amplitude analysis analytical angle of attack applied Astronautics baseline behavior bending bond buckling component composite compressive compressive strength configuration constant crack growth rate crack length criterion curve cycle damping displacement effect elastic energy Engineers equations evaluated experimental failure fatigue crack growth fibre finite element flaw flight Flight Dynamics flutter speed fracture mechanics fracture toughness frequency function inches increase incremental initial 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 plate predicted pressure problem procedure ratio response shear shear strength shear stress shell shown in Figure Shuttle specimens spectrum stiffened stiffness strain strain energy strength stress intensity factor surface technique tensile theory thickness tion titanium transonic tunnel values weight wing