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Longitudinal characteristics and aileron effectiveness of a midwing airplane from high-speed wind tunnel tests
Report presenting wind-tunnel tests of a 0.175-scale model of a midwing airplane in order to determine the high-speed longitudinal characteristics, to test devices for improving longitudinal control at high Mach numbers, and to determine the aileron effectiveness at high Mach numbers. Force and moment coefficients are computed from test data. Control forces, elevator angle, and aileron angle for several flight conditions are predicted.
Date:
September 29, 1944
Creator:
Hall, Charles F. & Mannes, Robert L.
System:
The UNT Digital Library