High-speed wind-tunnel investigation of high lift and aileron-control characteristics of an NACA 65-210 semi-span wing

Jack Fischel, Leslie E. Schneiter
Nov 1947

A high-speed wind-tunnel investigation was made of the aerodynamic characteristics at various Mach numbers of an NASA 65-210 semispan wing variously equipped with a 25-percent-chord full-span slotted flap and a 38-percent-semispan 20-percent-chord straight-sided ailaron.

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