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Calculation of the performance characteristics of a three-dimensional scramjet nozzle/afterbody system - MaRDI portal

Calculation of the performance characteristics of a three-dimensional scramjet nozzle/afterbody system

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Publication:1569354

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zbMath0962.76062MaRDI QIDQ1569354

M. K. Aukin, R. K. Tagirov

Publication date: 3 July 2000

Published in: Computational Mathematics and Mathematical Physics (Search for Journal in Brave)

zbMATH Keywords

viscous effects hypersonic aircraft three-dimensional scramjet nozzle flows

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Hypersonic flows (76K05)

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