AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter, and Limit-Cycle Oscillations
AIAA journal ; 40 , 4 ; 638-646
2002
Article (Journal)
English
British Library Conference Proceedings | 2001
|AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Damping Effects in Nonlinear Panel Flutter
Online Contents | 2000
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