ASD Technical Report, Numéro 61,Partie 645

aero aerodynamic heating aerodynamic influence coefficient aerospace aerothermo aerothermodynamics aerothermoelastic aircraft airfoil altitude analysis angle of attack approximation basic beam bending blunt body booster boundary layer camber characteristics computed configuration considerations control system cylinders deflections deformation discussed distribution duralumin dynamic pressure effects elastic engineering equations equilibrium experimental Figure flexible flight control flow frequency fuel heat transfer heating rates hypersonic inputs leading edge lift coefficient lifting pressure linear theory load Mach number materials matrix methods mission mode mode shapes NASA nondimensional nonlinear nose obtained order theory panel flutter parameters prediction present ratio re-entry reference requirements rigid scale shell shock shown slope solution spacecraft speed stability and control stagnation pressure static aeroelastic stiffness structural supersonic surface techniques temperature tests thermal stresses thermoelastic thickness tion truss unsteady velocity vibration wind tunnel wing ду дх