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Investigation of a Two-Step Nozzle in the Langley 11-Inch Hypersonic Tunnel

An investigation of four wings of square plan form at a Mach number of 6.9 in the Langley 11-inch hypersonic tunnel

An Investigation of Four Wings of Square Plan Form at a Mach Number of 6.86 in the Langley 11-Inch Hypersonic Tunnel

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

Published Year

• 1950-1959 (4) *

Subject

• Aerodynamics, Supersonic (1)
• Aerofoils (1)
• Charts, diagrams, etc (1)
• Drag (Aerodynamics) (1)
• Lift (Aerodynamics) (1)

Author

• McLellan, Charles H. (4) *
• Bertram, Mitchel H. (2)
• Dunning, Robert W. (1)
• Williams, Thomas W. (1)

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