Publication Date:
2019-07-11
Description:
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.
Keywords:
Aircraft Stability and Control
Type:
NACA-RM-L7H01-PT-3
Format:
application/pdf