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Stability and control characteristics obtained during demonstration of the Douglas X-3 research airplane

Richard Ellsworth Day, Jack Fischel

Abstract

Report presenting flight tests performed using the Douglas X-3 research airplane during the manufacturer's demonstration program and U.S. Air Force evaluation. Tests were performed over a range of Mach numbers and altitudes. Longitudinal, lateral, and directional stability and control data were obtained during steady and maneuvering flight and are compared with wind-tunnel and rocket-model data in this report.

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Available abstract

Key concepts: Airplane, Aeronautics, Longitudinal static stability, Mach number, Aerospace engineering, Rocket (weapon), Wind tunnel, Stability (learning theory)