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Computational Methods for Fluid Flow pp 267–309Cite as

Inviscid Compressible Flows

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Part of the book series: Springer Series in Computational Physics ((SCIENTCOMP))

Abstract

In the area of inviscid compressible flows there are a variety of practical problems that arise in everyday engineering applications. These include rocket nozzle flows, aircraft and missile engine inlet flows, reentry vehicle and rocket aerodynamics, blast fields generated by different types of energy release, and aircraft flow fields. One can, of course, continue the list, but these serve as examples whose discussion will adequately display the techniques for solving compressible-flow problems.

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Authors and Affiliations

  1. CNRS, Département de Mathématiques, Université de Nice, F-06000, Nice, France

    Roger Peyret

  2. Applied Physics Laboratory, Johns Hopkins University, Laurel, Maryland, USA

    Thomas D. Taylor

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  1. Roger Peyret
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  2. Thomas D. Taylor
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© 1983 Springer-Verlag New York Inc.

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Peyret, R., Taylor, T.D. (1983). Inviscid Compressible Flows. In: Computational Methods for Fluid Flow. Springer Series in Computational Physics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-85952-6_10

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  • DOI: https://doi.org/10.1007/978-3-642-85952-6_10

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-13851-8

  • Online ISBN: 978-3-642-85952-6

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