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-Foot

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 longitudinal-control characteristics of the complete model are presented in the present report with a limited analysis of the results.