A collection of technical papers: the 34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Adaptive Structures Forum ; April 19-22, 1993, Part 4
American Institute of Aeronautics and Astronautics, 1993 - Aerodynamics
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aeroelastic AIAA aircraft algorithm analytical angle applied approximate axial beam behavior bending boundary conditions buckling load calculated coefficients Composite Materials computed configuration constitutive equations constraint coordinates crack growth curve cutout cylinder damage damping defined deflection deformation delamination design variables displacement displacement vector dual-wall systems effect eigenvalue elastic energy equations error excitation experimental factor failure fiber finite element analysis finite element method flexible flutter formulation frequency function geometric impact imperfection initial Integrated iterations laminate layer layup linear Lyapunov equation Mechanics method modal mode shapes modulus neural network node nonlinear notched obtained Optimal Design PANDA2 panel parameters plies postbuckling predicted pressure wall plate problem response sensitivity derivatives shape optimization shear shown in Figure simulation solution specimen stiffness matrix strain rate stress structural surface temperature thermal thermal conductivity thickness tion transverse truss values variation vector velocity Vibration viscoelastic wing