See also Engineering Index 1947 p 56.
Effects of mach number up to 0.34 and Reynolds number up to 8×106 on maximum lift coefficient of wing of NACA 66-series airfoil sections
Nat Advisory Committee Aeronautics -- Tech Note
1950
43 pages
Illustrations, Diagrams
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1947
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