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On the stand-off distance of detached shock waves in internal transonic flows

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Fluid- and Gasdynamics

Part of the book series: Acta Mechanica ((ACTA MECH.SUPP.,volume 4))

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Summary

The stand-off distance of detached shock waves in internal transonic flows depends not only on the shape of the profile (body) in front of which the shock occurs: it is strongly affected by the channel geometry. The front shock waves can easily be misinterpreted with shock waves terminating the region of supersonic flow in the channel.

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References

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Author information

Authors and Affiliations

  1. Institute of Thermomechanics, Czech Academy of Sciences, Dolejškova 5, CS-18200, Praha 8, Czech Republic

    Dr.-Ing. R. Dvořák DrSc.

Authors
  1. Dr.-Ing. R. Dvořák DrSc.
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Editors and Affiliations

  1. Institut für Strömungslehre und Strömungsmaschinen, Universität Karlsruhe (TH), Karlsruhe, Federal Republic of Germany

    G. H. Schnerr , R. Bohning  & W. Frank ,  & 

  2. Fachbereich Maschinenbau, Fachhochschule Offenburg, Offenburg, Federal Republic of Germany

    K. Bühler

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© 1994 Springer-Verlag

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Dvořák, R. (1994). On the stand-off distance of detached shock waves in internal transonic flows. In: Schnerr, G.H., Bohning, R., Frank, W., Bühler, K. (eds) Fluid- and Gasdynamics. Acta Mechanica, vol 4. Springer, Vienna. https://doi.org/10.1007/978-3-7091-9310-5_16

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  • DOI: https://doi.org/10.1007/978-3-7091-9310-5_16

  • Publisher Name: Springer, Vienna

  • Print ISBN: 978-3-211-82495-5

  • Online ISBN: 978-3-7091-9310-5

  • eBook Packages: Springer Book Archive

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