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Experimental determination of the recovery factor and analytical solution of the conical flow field for a 20 ̊included angle cone at Mach numbers of 4.6 and 6.0 and stagnation temperatures to 2600 ̊R

Title:Experimental determination of the recovery factor and analytical solution of the conical flow field for a 20 ̊included angle cone at Mach numbers of 4.6 and 6.0 and stagnation temperatures to 2600 ̊R
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Note:National Aeronautics and Space Administration, 1961
  
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Subject:Aerodynamics, Hypersonic
Subject:Boundary layer
Subject:Cone -- Aerodynamics
Subject:Energy transfer
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