Investigation made in 7 by 10-ft wind tunnel and in variable density wind tunnel of airfoil with various slotted flap arrangements, in order to determine airfoil section aerodynamic characteristics as affected by flap shape, slot shape, and flap location. (10¢)
Wind-tunnel investigation of N.A.C.A. 23012 airfoil with various arrangements of slotted flaps
Nat Advisory Committee Aeronautics -- Report
1939
31 pages
Bibliography
Report
English
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Engineering Index Backfile | 1940
|Pressure distribution over N.A.C.A. 23012 airfoil with slotted and plain flaps
Engineering Index Backfile | 1938
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