Free-flight investigation at transonic and supersonic speeds of the rolling effectiveness of a partial-span aileron on an inversely tapered sweptback wing

H. Kurt Strass, E. M. Fields, E. D. Schult
naca-rm-l50b08
May 1950


An investigation of the rolling effectiveness at transonic and supersonic speeds of an inversely tapered sweptback wing having a 10-percent-thick cambered airfoil section and outboard partial-span controls has been made by means of rocket-propelled test vehicles.

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