Theoretical Lift and Damping in Roll of Thin Sweptback Wings of Arbitrary Taper and Sweep at Supersonic Speeds. Subsonic Leading Edges and Supersonic Trailing Edges.
Theoretical lift and damping in roll of thin sweptback wings of arbitrary taper and sweep at supersonic speeds. Subsonic leading edges and supersonic trailing edges
Nat Advisory Committee Aeronautics -- Tech Note
1949
40 pages
Diagrs, Charts
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1950
|Engineering Index Backfile | 1949
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