An Investigation Of The Aerodynamic Characteristics Of An 0.08-scale Model Of The Chance Vought Xf7u-1 Airplane In The Langley Hig
by Nasa Technical Reports Server (ntrs)
2021-01-04 19:43:47
An Investigation Of The Aerodynamic Characteristics Of An 0.08-scale Model Of The Chance Vought Xf7u-1 Airplane In The Langley Hig
by Nasa Technical Reports Server (ntrs)
2021-01-04 19:43:47
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 basic lateral ...
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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 basic lateral stability characteristics of the complete model with undeflected control surfaces are presented in the present report with a very limited analysis of the results.
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