Flight data pertinent to buffeting and maximum normal-force coefficient of the Douglas X-3 research airplane
Description:
Report presenting the X-3 airplane, which has a straight 4.5-percent-thick wing of modified hexagonal section, which has been flown to maximum wing normal-force coefficients in the Mach number range from 0.7 to 1.1 at an average altitude of 30,000 feet. Measurements were made of airplane and wing-panel maximum normal-force coefficients and of some buffeting characteristics.
Date:
November 20, 1957
Creator:
Baker, Thomas F.; Martin, James A. & Scott, Betty J.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department