Wind-tunnel tests of a Clark Y wing having split flaps with gaps (1938)
NASA Technical Reports Server (NTRS) · leaf 6
N.A.C.A. Teohnioal Mote No. 650 Fig. 2 o … Angle of attack, cC ,deg. rigure 2.- Lift, drag, and center-of-preesure characteristic* of Olark Y wing with full-span aplit flaps and gap "between flap and wing.
NASA Technical Reports Server (NTRS)
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