Lift, drag, pitching moment, and flap hinge moment data obtained for wing with various flaps deflected up to 60°.
Wind-tunnel investigation at low speed of unswept untapered semispan wing of aspect ratio 3.13 equipped with various 35-percent-chord plain flaps
Nat Advisory Committee Aeronautics -- Tech Note
1950
27 pages
Illus, Diagrs, Charts, Tables
Aufsatz (Zeitschrift)
Englisch
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