Effects of compressibility on lift and load characteristics of tapered wing of NACA 64-210 airfoil sections up to Mach number of 0.60.
Effects of compressibility on lift and load characteristics of tapered wing of NACA 64-210 airfoil sections up to Mach number of 0.60
Nat Advisory Committee Aeronautics -- Tech Note
1949
48 pages
Illus, Charts, Diagrs
Report
English
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Engineering Index Backfile | 1948
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