Results of measurements of maximum lift and buffeting intensities obtained during flight investigation of the Northrop X-4 research airplane
Description: The variation of the intensity of buffeting experienced throughout the operational region of the semitailless Northrop X-4 airplane and the values of maximum and peak normal-force coefficients in the Mach number range from 0.42 to 0.92 have been determined. The results are compared with data obtained with the swept-wing Douglas D-558-II airplane.
Date: August 20, 1953
Creator: Baker, Thomas F.
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