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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

Title: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
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Note:National Advisory Committee for Aeronautics, 1952
  
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Subject:Aerodynamics, Supersonic
Subject:Base flow (Aerodynamics)
Subject:Body of revolution
Subject:Drag (Aerodynamics)
Subject:Reynolds number
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