Effect of slot shape, flap position, and flap deflection on section; aerodynamic characteristics determined and discussed.
Wind-tunnel investigation of N,A,C,A, 23021 airfoil with two arrangements of 40-percent-chord slotted flap
Nat Advisory Committee Aeronautics -- Tech Note
1939
11 pages
Bibliography, 11 Supp sheets
Report
English
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Wind-tunnel investigation of N.A.C.A. 23021 airfoil with various arrangements of slotted flaps
Engineering Index Backfile | 1939
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