Cambered wing was tested in transonic wind tunnel with indented and nonindented body, and similar plane wing with indented body; conical camber reduced and delayed wing tip stall and reduced severity of its associated longitudinal instability; other results.
Transonic aerodynamic loading characteristics of wing-body-tail combination having 52.5° sweptback wing of aspect ratio 3 with conical wing camber and body indentation for design mach number of root 2
NASA -- Tech Note
1961
99 pages
Report
English
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