Numerical Simulation Of Supersonic Compression Corners And Hypersonic Inlet Flows Using The Rplus2d Code

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Language: en
Pages: 30

Numerical Simulation of Supersonic Compression Corners and Hypersonic Inlet Flows Using the Rplus2d Code

Authors: National Aeronautics and Space Adm Nasa

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Type: BOOK - Published: 2018-12-29 - Publisher: Independently Published

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A two-dimensional computational code, PRLUS2D, which was developed for the reactive propulsive flows of ramjets and scramjets, was validated for two-dimensional