Most promising arrangement of full span lift flap and plain aileron combination tested, both for high lift and lateral control, was rectangular wing with 0.20cw flap deflected 60 at 0.90cw location with 0.10cw semi-span ailerons.
Wind-tunnel investigation of rectangular and tapered N.A.C.A. 23012 wings with plain ailerons and full-span split flaps
Nat Advisory Committee Aeronautics -- Tech Note
1938
11 pages
9 Supp sheets, Bibliography
Report
English
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Engineering Index Backfile | 1938
|Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps
Engineering Index Backfile | 1937
|Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps
Engineering Index Backfile | 1937
|