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Effect of a variable-geometry diffuser on the operating characteristics of a helium tunnel designed for a mach number in excess of 20

Title:Effect of a variable-geometry diffuser on the operating characteristics of a helium tunnel designed for a mach number in excess of 20
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Note:National Aeronautics and Space Administration, 1960
  
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Subject:Conical nozzles
Subject:Flow characteristics
Subject:Helium
Subject:Mach number
Subject:Pressure ratio
Subject:Reynolds number
Subject:Supersonic diffusers
Subject:Supersonic speed
Subject:Supersonic wind tunnels
Subject:Variable geometry structures
Subject:Viscosity
Subject:Wind tunnel tests
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