Theoretical analysis based on linearized theory for supersonic flow; two cases treated: in one, flap extended outboard from center of wing and in other, flap extended inboard from wing tip.
Characteristics of thin triangular wings with constant-chord partial-span control surfaces at supersonic speeds
Nat Advisory Committee Aeronautics -- Tech Note
1948
43 pages
Aufsatz (Zeitschrift)
Englisch
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