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Thirteenth International Conference on Numerical Methods in Fluid Dynamics pp 130–134Cite as

A three-dimensional pressure flux-split RNS formulation: Application to subsonic/supersonic flow in inlets and ducts

  • Upwind and Characteristic Type Methods
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Part of the book series: Lecture Notes in Physics ((LNP,volume 414))

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References

  1. Rubin, S.G. and Khosla, P.K., “A Review of Reduced Navier-Stokes Computations for Compressible Viscous Flows”, J. Comput. Syst. in Eng., 1, pp. 549–562, 1990.

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Authors and Affiliations

  1. Department of Aerospace Engineering and Engineering Mechanics, University of Cincinnati, 45221, Cincinnati, Ohio

    H. S. Pordal, S. G. Rubin & P. K. Khosla

Authors
  1. H. S. Pordal
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  2. S. G. Rubin
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  3. P. K. Khosla
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M. Napolitano F. Sabetta

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© 1993 Springer-Verlag

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Pordal, H.S., Rubin, S.G., Khosla, P.K. (1993). A three-dimensional pressure flux-split RNS formulation: Application to subsonic/supersonic flow in inlets and ducts. In: Napolitano, M., Sabetta, F. (eds) Thirteenth International Conference on Numerical Methods in Fluid Dynamics. Lecture Notes in Physics, vol 414. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3-540-56394-6_202

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  • DOI: https://doi.org/10.1007/3-540-56394-6_202

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-56394-5

  • Online ISBN: 978-3-540-47551-4

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