Scale and Turbulence Effects on Lift and Drag Characteristics of NACA 653-418, a = 1.0 Airfoil Section. (Advance Confidential Report L4H11)
Scale and turbulence effects on lift and drag characteristics of NACA 653-418, a = 1.0 airfoil section
Nat Advisory Committee Aeronautics -- Wartime Report
1944
9 pages
13 Supp plates
Report
Englisch
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