AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Finite Element Modal Formulation for Hypersonic Panel Flutter Analysis with Thermal Effects
AIAA journal ; 42 , 4
2004
Article (Journal)
English
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Damping Effects in Nonlinear Panel Flutter
Online Contents | 2000
|Finite Element Modal Formulation for Hypersonic Panel Flutter Analysis with Thermal Effects
British Library Conference Proceedings | 2003
|