Data presented in form of curves of sections lift, drag, and pitching moment coefficients for airfoil with flap deflected but with ailerons neutral, and of rolling, yawing, and hinge moment coefficients for rectangular wing of aspect ratio 6 with semi-span aileron and full span flap.
Wind-tunnel test of three lateral-control devices in combination with full-span slotted flap on N.A.C.A. 23012 airfoil
Nat Advisory Committee Aeronautics -- Tech Note
1938
11 pages
6 Supp sheets, Bibliography
Report
English
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Engineering Index Backfile | 1938
|Pressure distribution over N.A.C.A. 23012 airfoil with N.A.C.A. 23012 external-airfoil flap
Engineering Index Backfile | 1938
|Tests of N.A.C.A 23012 airfoil with slotted deflector flap
Engineering Index Backfile | 1939
|Engineering Index Backfile | 1939
|