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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
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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)