With split flaps of equal length both wings had same CLmax; if 30% of flap outer span were removed for installation of ailerons, reduction in CLmax of tapered wings with flaps might be expected of order of 4 to 7%; results of tests using ailerons of same span.
Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps
Nat Advisory Committee Aeronautics -- Report
1937
9 pages
Bibliography
Report
English
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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
|Wind-tunnel investigation of wings with ordinary ailerons and full-span external-airfoil flaps
Engineering Index Backfile | 1937
|