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• W3196397764 abstract "In this study, we obtain the comparative analysis of methods of quick approximate analytical prediction of Mach shock height in planar steady supersonic flows (for example, in supersonic jet flow and in narrowing channel between two wedges), that are developed since the 1980s and being actively modernized now. A new analytical model based on flow averaging downstream curved Mach shock is proposed, which seems more accurate than preceding models, comparing with numerical and experimental data." @default.
• W3196397764 created "2021-09-13" @default.
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• W3196397764 date "2021-08-28" @default.
• W3196397764 modified "2023-09-27" @default.
• W3196397764 title "Approximate Analytical Models of Shock-Wave Structure at Steady Mach Reflection" @default.
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• W3196397764 doi "https://doi.org/10.3390/fluids6090305" @default.
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