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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