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Effects of Reynolds number and model support on the supersonic aerodynamic chacteristics of a 140° included-angle cone /

Title:Effects of Reynolds number and model support on the supersonic aerodynamic chacteristics of a 140° included-angle cone /
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Author:
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Note:Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974
  
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Subject:Wind tunnel models
Subject:Reynolds number
Subject:Aerodynamics, Supersonic
Subject:Cone
Subject:Wind tunnel apparatus
Subject:Pressure measurements
Subject:Aerodynamic interference
Subject:Wind tunnel tests
Subject:Static aerodynamic characteristics
Subject:Conical bodies
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