1. Aeroelastic stability of orthotropic heterogeneous thin panels in vicinity of flutter critical boundary.1. Simply supported panels;Librescu;J. Méc.,1965
2. Aeroelastic stability of orthotropic heterogeneous thin panels in the vicinity of the flutter critical boundary, II (boundary conditions influence on flutter critical boundary character considering nonlinearities of physical nature);Librescu;J. Méc.,1967
3. Comparing theory and experiment for the supersonic flutter of circular cylindrical shells;Olson;AIAA J.,1967
4. Supersonic flutter of circular cylindrical shells subjected to internal pressure and axial compression;Olson;AIAA J.,1966
5. Nonlinear supersonic flutter of circular cylindrical shells;Amabili;AIAA J.,2001