Boom is due to effects of body volume, wing volume, wing incidence or lift, and wing-body interference; contribution in far field of each of factors can be represented as that of equivalent body of revolution; concept is developed to investigate possibilities of using interference, to reduce or suppress boom due to lift; results of wind tunnel experiments.
Supersonic boom of wing-body configurations
J Aerospace Sciences
Journal of Aerospace Science ; 28 , n 4
1961
8 pages
Article (Journal)
English
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FLUTTER OF SUPERSONIC WING-BODY CONFIGURATIONS
AIAA | 1963
|British Library Conference Proceedings | 2002
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