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Investigation of the aerodynamic characteristics at high supersonic Mach numbers of a family of delta wings having double-wedge sections with the maximum thickness at 0.18 chord

An Investigation of the Characteristics of the NACA RM-10 (With and Without Fins) in the Langley 11-Inch Hypersonic Tunnel at a Mach Number of 6.9

Published Year

• 1950-1959 (2) *

Subject

• Aerodynamics, Supersonic (1)
• Airplanes--Wings, Triangular (1)
• Charts, diagrams, etc (1)
• Mach number (1)
• Wedges--Aerodynamics (1)

Author

• McCauley, William D. (2) *
• Bertram, Mitchel H. (1)

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