Theoretical Lift and Damping in Roll at Supersonic Speeds of Thin Sweptback Tapered Wings with Streamwise Tips, Subsonic Leading Edges, and Supersonic Trailing Edges.
Theoretical lift and damping in roll at supersonic speeds of thin sweptback tapered wings with streamwise tips, subsonic leading edges, and supersonic trailing edges
Nat Advisory Committee Aeronautics -- Reports
1950
16 pages
Diagrams, Graphs
Report
Englisch
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Engineering Index Backfile | 1951
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