AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Nonlinear Flutter of Composite Panels Under Yawed Supersonic Flow Using Finite Elements
AIAA journal ; 37 , 9
1999
Aufsatz (Zeitschrift)
Englisch
Nonlinear Flutter of Curved Panels Under Yawed Supersonic Flow Using Finite Elements
British Library Conference Proceedings | 2003
|