Wind-tunnel investigation of the use of leading-edge and trailing-edge area-suction flaps on a 13-percent-thick straight wing and fuselage model

Holzhauser, Curt A.

Lift, drag, and pitching-moment coefficents were measured on a straight-wing model that had a full-span leading-edge flap and a partial-span trailing-edge flap, each with porous area at the knee.

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