Preliminary results from flight measurements in gradual-turn maneuvers of the wing loads and the distribution of load among the components of a Boeing B-47A airplane
Description: Report presenting an analysis of some strain-gage measurements of the loads carried by the wing and horizontal tail of a Boeing B-47A airplane during gradual-turn maneuvers for a variety of altitudes and Mach numbers. Results regarding the wing-load center of pressure, component loads, component-force coefficients, and fraction of the wing-fuselage load carried by the wing are provided.
Date: June 27, 1955
Creator: Cooney, T. V.; Andrews, William H. & McGowan, William A.
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Partner: UNT Libraries Government Documents Department