Effects of spoiler-slot-deflector control on the aerodynamic characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with the outer wing panels swept back 75° /
by Gerald V. Foster.

APA Citation

Foster, G. V., United States. National Aeronautics and Space Administration. (1960). Effects of spoiler-slot-deflector control on the aerodynamic characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with the outer wing panels swept back 75°. Washington [D.C.]: National Aeronautics and Space Administration.

MLA Citation

Foster, Gerald V, and United States. National Aeronautics and Space Administration. Effects of Spoiler-slot-deflector Control On the Aerodynamic Characteristics At a Mach Number of 2.01 of a Variable-wing-sweep Configuration With the Outer Wing Panels Swept Back 75°. Washington [D.C.]: National Aeronautics and Space Administration, 1960.