Wing-load measurements at supersonic speeds of the Douglas D-558-II research airplane
Description:
From Summary: "Flight measurements of the aerodynamic wing loads on the D-558-II airplane have been made in the Mach number range from 1.0 to 2.0. Nonlinear wing-panel characteristics occurred with variations in angle of attack. These nonlinear characteristics were apparent primarily at the lower supersonic speeds."
Date:
March 30, 1955
Creator:
Robinson, Glenn H.; Cothren, George E., Jr. & Pembo, Chris
Item Type:
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