A collection of technical papers: AIAA/ASME/ASCE/AHS 23rd Structures, Structural Dynamics and Materials Conference, May 10-12, 1982, New Orleans, Louisiana, Volume 2
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AIAA NO PAGE
Structural Design of Integral Tankage for Advanced Space Trans
A Damage Induced Aeroelastic Failure Mode Involving Combination
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aerodynamic aeroelastic AIAA aircraft airfoil airplane amplitude analytical angle of attack angle-of-attack approximation beam bending blade buckling cable tray calculated chord coefficients configuration control law critical damage tolerance damping deflection derivatives design variables displacement divergence durability and damage dynamic pressure effects eigenvalues elastic axis equation experimental finite element flexible flight flutter boundary flutter speed force frequency function fuselage geometric impact increase integral iteration Lagrange multipliers linear load LTRAN2-NLR LTRAN3 Mach number mass MBB A-3 method modal mode shapes motion NACA NASA NASTRAN nodes nondimensional nonlinear obtained optimal oscillation parameters pitch predicted problem procedure ratio response rotating shaft shear shear modulus shown in Figure solution SPAR stability static structural supercritical supercritical airfoil Supercritical Wing swept wing Table technique tion torsion transonic unstable unsteady values vector velocity vibration weight wind tunnel wing winglet