1957•Unpublished venueRequires access

Flight Data Pertinent to Buffeting and Maximum Normal-force Coefficient of the Douglas X-3 Research Airplane

Thomas F Baker, James A. Martin, Betty J. Scott

Abstract

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.

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Key concepts: Airplane, Wing, Aeroelasticity, Wing loading, Mach number, Range (aeronautics), Aerospace engineering, Altitude (triangle)