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 Tunnel: Part III Longitudinal-Control Characteristics Ted No. NACA De308
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 Tunnel: Part III Longitudinal-Control Characteristics Ted No. NACA De308
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.
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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.
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