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3-Dimensional upwind Euler solver using kinetic flux vector splitting method

  • Upwind and Characteristic Type Methods
  • Conference paper
  • First Online:
Thirteenth International Conference on Numerical Methods in Fluid Dynamics

Part of the book series: Lecture Notes in Physics ((LNP,volume 414))

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References

  1. Deshpande S.M. “Kinetic theory based new upwind methods for inviscid compressible flows”,AIAA Paper 86-0275,1986.

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  4. Thomas P.D. and Middlecoff J.F.,AIAA Journal 18, p 652, 1980

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  5. Borrel M., Montagne J K., Diet J., Guillen Ph. and Lorden J., “Upwind scheme for computing supersonic flows around a tactical missile”, Rech. Aerosp-n, 1988.

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Author information

Authors and Affiliations

  1. Department of Aerospace Engineering, I.I.Sc., 560012, Bangalore

    S. Deshpande

  2. Defence Research & Development Laboratory, 500258, Hyderabad, India

    S. Sekar, M. Nagarathinam, R. Krishnamurthy & P. Sinha

Authors
  1. S. Deshpande
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  2. S. Sekar
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  3. M. Nagarathinam
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  4. R. Krishnamurthy
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  5. P. Sinha
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  6. P. Kulkarni
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Editor information

M. Napolitano F. Sabetta

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© 1993 Springer-Verlag

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Deshpande, S., Sekar, S., Nagarathinam, M., Krishnamurthy, R., Sinha, P., Kulkarni, P. (1993). 3-Dimensional upwind Euler solver using kinetic flux vector splitting method. 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_197

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  • DOI: https://doi.org/10.1007/3-540-56394-6_197

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-56394-5

  • Online ISBN: 978-3-540-47551-4

  • eBook Packages: Springer Book Archive

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