Theoretical supersonic characteristics of inboard trailing-edge flaps having arbitrary sweep and taper. Mach lines behind flap leading and trailing edges.
Theoretical supersonic characteristics of inboard trailing-edge flaps having arbitrary sweep and taper. Mach lines behind flap leading and trailing edges
Nat Advisory Committee Aeronautics -- Tech Note
1950
39 pages
Diagrs, Graphs
Report
Englisch
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Engineering Index Backfile | 1950
|Engineering Index Backfile | 1952
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