A Collection of Technical Papers, Part 2 |
Contents
Paper No Title and Author Page | 575 |
SESSION 33Dynamics | 580 |
continued | 583 |
Copyright | |
37 other sections not shown
Common terms and phrases
adhesive aerodynamic aeroelastic AIAA aircraft algorithm analysis analytical angle applied beam bending boundary conditions calculated coefficient collective pitch components composite Composite Materials compression computational configuration constraints contact angle crack damage damping deflections deformation delamination derivatives design variables displacement distribution effect eigenvalue elastic Engineering equations error estimation experimental fiber Figure finite element finite element method flutter formulation fracture full state feedback geometry handling qualities heating Helicopter Rotor hub shear in-plane integrated Journal laminate leading edge linear mass material measured Mechanics method modal modal test mode shapes modulus NASA natural frequencies nodes Nondimensional nonlinear obtained optimization parameters phugoid plate predicted present problem procedure ratio reduced response rotation second order observer shown in Fig solution specimen stability stiffness matrix strain stress Structural Dynamics surface technique temperature theory thermal tion torsional transverse values vector velocity Vibration weight wing Young's modulus zero