Representation of lift for fairly general family of wing body configurations (with no afterbody) in linearized supersonic flow considered over entire range of parameters; bracketing limits of lift obtained simply, using most elementary considerations when interpretation of these limits is recognized.
Supersonic wing-body lift
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 18 , n 4
1951
12 pages
Aufsatz (Zeitschrift)
Englisch
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