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A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel

Spinning and related problems at high angles of attack for high-speed airplanes

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 (3)

Subject

• Supersonic planes (3) *
• Aerodynamics, Supersonic (1)
• Airplanes--Control (1)
• Airplanes--Fuselage (1)
• Charts, diagrams, etc (1)
• Fighter planes (1)
• Spin (Aerodynamics) (1)
• Stability of airplanes, Longitudinal--Testing (1)
• Stalling (Aerodynamics) (1)
• Yawing (Aerodynamics)--Testing (1)

Author

• D'Aiutolo, Charles T. (1)
• Hasel, Lowell E. (1)
• Klinar, Walter J. (1)
• Mason, Homer P. (1)
• Sinclair, Archibald R. (1)

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