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The Use of Suction to Prevent Shock-Induced Separation in a Nozzle

Normal force, center of pressure, and zero-lift drag of several ballistic-type missiles at Mach numbers of 4.05

Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form: Longitudinal and Lateral Control Characteristics

Factors affecting the maximum lift-drag ratio at high supersonic speeds

Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04

Published Year

• 1950-1959 (5)

Subject

• Charts, diagrams, etc (2)
• Drag (Aerodynamics) (2)
• Aerodynamics, Supersonic (1)
• Aerofoils (1)
• Airplanes--Wings, Trapezoidal (1)
• Airplanes--Wings, Triangular (1)
• Ballistic missiles (1)
• Boundary layer (1)
• Lift (Aerodynamics) (1)
• Rockets (Aeronautics)--Models (1)
• Turbulent boundary layer (1)

Author

• Dunning, Robert W. (5) *
• McLellan, Charles H. (1)
• Smith, Fred M. (1)
• Sterrett, James R. (1)
• Ulmann, Edward F. (1)

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