Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness at supersonic speeds of a 30-percent chord, 50-percent semispan elevon as a lateral control device

Robert N. Olson, Merrill H. Mead
naca-rm-a50k07
Jan 1951

The effectiveness of a 50-percent-semispan, constant-percent-chord elevon and of upper-surface spoilers as lateral-control devices for a wing-fuselage combination employing a wing swept back 63 degrees has been determined experimentally for the range of Mach numbers from 1.2 to 1.7 at a Reynolds number of 1.5 million.

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