Flutter Analysis of Composite Wings Using an Exact Dynamic Stiffness Matrix Method
Conference; Adaptive structures forum, Structures, structural dynamics and materials ; 1995 ; New Orleans; LA
1995-01-01
9 pages
5; pts
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Aeroelastic Optimization of High Aspect Ratio Wings Using an Exact Dynamic Stiffness Matrix Method
British Library Conference Proceedings | 1994
|Flutter Characteristics of Laminated Composite Wings
Online Contents | 1996
|A unified flutter analysis for composite aircraft wings
AIAA | 1984
|