An Investigation of the Aerodynamic Characteristics of an 0.08-Scale Model of the Chance Vought Xf7u-1 Airplane in the Langley High-Speed 7- By 10-Foo

Tests have been conducted in the Langley high-speed 7- by 10-foot tunnel over a Mach number range from 0.40 to 0.91 to determine the stability and control characteristics of an 0.08-scale model of the Chance Vought XF7U-1 airplane. The aileron characteristics of the complete model are presented in the present report with a very limited analysis of the results.