AIAA-2002-5547 Sonic Boom Reduction Using an Adjoint Method for Wing-Body Configurations in Supersonic Flow
Symposium; 9th, Multidisciplinary analysis and optimization ; 2002 ; Atlanta, GA
2002-01-01
10 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Sonic Boom Reduction via Remote Inverse Adjoint Approach AIAA Paper
British Library Conference Proceedings | 2007
|Supersonic boom of wing-body configurations
Engineering Index Backfile | 1961
|Sonic Boom Reduction via Remote Inverse Adjoint Approach
AIAA | 2007
|