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Development and testing of a new optimum design code for hypersonic wind tunnel nozzles, including boundary layer, turbulence, and real gas effects /

Ralph Tolle, Air Force Wright Aeronautical Laboratories. issuing body., Air Force Flight Dynamics Laboratory (U.S.). sponsor.

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Abstract

"Final Report for 07/01/92--11/19/95."

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What this paper is about

"Final Report for 07/01/92--11/19/95."

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Available abstract

"Final Report for 07/01/92--11/19/95."

Key concepts: Nozzle, Mach number, Wind tunnel, Hypersonic speed, Inviscid flow, Aerospace engineering, Turbulence, Engineering

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Development and testing of a new optimum design code for hypersonic wind tunnel nozzles, including boundary layer, turbulence, and real gas effects / — Research Paper | ScholarLens