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Investigation of the variation with Reynolds number of the base, wave, and skin-friction drag of a parabolic body of revolution (NACA RM-10) at Mach numbers of 1.62, 1.93, and 2.41 in the Langley 9-inch supersonic tunnel

Investigation of the aerodynamic characteristics of the NACA RM-10 missile (with fins) at a Mach number of 1.62 in the Langley 9-inch supersonic tunnel

Published Year

• 1950-1959 (2)

Subject

• Aerodynamics, Supersonic (2) *
• Base flow (Aerodynamics) (1)
• Body of revolution (1)
• Drag (Aerodynamics) (1)
• Guided missiles--Aerodynamics (1)
• Reynolds number (1)

Author

• Coletti, Donald E. (2) *
• Bromm, August F. (1)
• Love, Eugene S. (1)

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