Lift and pitching moment at supersonic speeds due to constant vertical acceleration for thin sweptback tapered wings with streamwise tips -- Supersonic leading and trailing edges.
Lift and pitching moment at supersonic speeds due to constant vertical acceleration for thin sweptback tapered wings with streamwise tips -- Supersonic leading and trailing edges
NACA -- Tech Note
1954
67 pages
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1951
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