Effects of Flow Angularity on Nonlinear Supersonic Flutter of Composite Panels
Conference, Structures, structural materials and dynamics ; 1999 ; St Louis; MO
1999-01-01
10 pages
Nos 99-1202 to 99-1613 with gaps
Conference paper
English
structures , AIAA , ASME , ASCE
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Flutter analysis of composite panels in supersonic flow
AIAA | 1990
|Supersonic flutter of composite sandwich panels
Tema Archive | 1992
|Supersonic Flutter of Composite Sandwich Panels
AIAA | 1992
|