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Preliminary results of the flight investigation between Mach numbers of 0.80 and 1.36 of a rocket-powered model of a supersonic airplane configuration having a tapered wing with circular-arc sections and 40©� sweepback

Published Year

• 1950-1959 (1)

Subject

• Stability of airplanes, Longitudinal--Testing (1) *
• Supersonic planes (1)
• Yawing (Aerodynamics)--Testing (1)

Author

• D'Aiutolo, Charles T. (1)
• Mason, Homer P. (1) *

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