Theoretical calculations of lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tips -- Subsonic leading edges.
Theoretical calculations of lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tips -- Subsonic leading edges
Nat Advisory Committee Aeronautics -- Tech Note
1950
33 pages
Diagrs, Charts
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1950
|Engineering Index Backfile | 1951
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