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Flight Test of the Lateral Stability of a 0.133-Scale Model of the Convair Xfy-1 Airplane with Windmilling Propellers at Mach Numbers from 0.70 to 1.1
James a. Hollinger
Paperback. BiblioGov 2013-07-22.
ISBN 9781289222826
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Förlagets beskrivning
A flight test of a rocket-propelled model of the Convair XFY-1 airplane was conducted to determine the lateral stability and control characteristics, The 0.133-scale model had windmilling propellers for this test, which covered a Mach number range of O.70 to 1.12. The center of gravity was located at 13.9 percent of the mean aerodynamic chord. The methods of analysis included both a solution by vector diagrams and simple one- and two-degree-of-freedom methods. The model was both statically and dynamically stable throughout the speed range of the testa The roll damping was good, and the slope of the side-force curve varied little with speed. The rudder was effective throughout the test speed range, although it was reduced to about 43 percent of its subsonic value at supersonic speeds
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Flight Test of the Lateral Stability of a 0.133-Scale Model of the Convair Xfy-1 Airplane with Windmilling Propellers at Mach Numbers from 0.70 to 1.1
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