Wind-tunnel investigation of NACA 23012 airfoil with two sizes of balanced split flap. (Advance Confidential Report Nov 1940)
Wind-tunnel investigation of NACA 23012 airfoil with two sizes of balanced split flap
Nat Advisory Committee Aeronautics -- Wartime Report
1940
13 pages
20 Supp plates
Report
Englisch
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Wind-tunnel investigation of NACA 23012 airfoil with 0.30-airfoil-chord double slotted flap
Engineering Index Backfile | 1943
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