Aerodynamic influence of wings on tailplane loads; downwash induced in plane of symmetry of aircraft when wings have straight leading edges whose sweepback is such that they are subsonic in supersonic main stream; downwash due to delta wing at incidence, having simple triangular planform, case of swallow tail wings.
Note on evaluation of supersonic downwash integral
Aeronautical Quarterly
Aeronautical Quarterly ; 5 , Part 2
1954
8 pages
Aufsatz (Zeitschrift)
Englisch
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