THREE-DIMENSIONAL HYPERSONIC GAS FLOW OVER A SLENDER WING.

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Abstract

The article examines examples illustrating the semi-inverse method, devised by the author for solving the steady-state problem of hypersonic gas flow over a slender wing.

Original languageEnglish
Pages (from-to)47-52
Number of pages6
JournalFluid mechanics. Soviet research
Volume10
Issue number1
Publication statusPublished - 1 Jan 1981

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  • Engineering(all)

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