Investigations carried out in N.A.C.A. 7-ft by 10-ft wind tunnel show aerodynamic advantages of aileron-flap combination appear to outweigh probable design difficulties.
Wind-tunnel investigation of wings with ordinary ailerons and full-span external-airfoil flaps
Nat Advisory Committee Aeronautics -- Report
1937
22 pages
Bibliography
Report
English
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Wind-tunnel investigation of wings with ordinary ailerons and full-span external-airfoil flaps
Engineering Index Backfile | 1937
|Wind-tunnel investigation of wings with ordinary ailerons and full-span external-airfoil flaps
Engineering Index Backfile | 1937
|Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps
Engineering Index Backfile | 1937
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