Effects of Reynolds Number and Leading-Edge Roughness on Lift and Drag Characteristics of NACA 653-418, a = 1.0 Airfoil Section (Confidential Bul L5J04).
Effects of Reynolds number and leading-edge roughness on lift and drag characteristics of NACA 653-418, a = 1.0 airfoil section
Nat Advisory Committee Aeronautics -- Wartime Report
1945
7 pages
8 Supp plates
Report
Englisch
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Section characteristics of NACA 0006 airfoil with area suction near leading edge
Engineering Index Backfile | 1954
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