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Transonic and supersonic flow calculations around aircrafts using a multidomain Euler code

  • Domain Decomposition Methods
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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. Ni R.H., A Multiple-Grid Scheme for Solving the Euler Equations, AIAA J., vol. 20, n° 11, 1982.

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  3. Couaillier V., Multigrid Methods for Solving Euler and Navier-Stokes Equations in two and three Dimensions, Proceedings of the eigth GAMM-Conference on Numerical Methods in Fluid Dynamics, Notes on Numerical Fluid Mechanics, Vol. 29. Edited by Pieter Wesseling, Vieweg, Braunschweig, 1990.

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Authors and Affiliations

  1. ONERA BP 72, 92322, Chatillon, France

    V. Couaillier, R. Grenon & N. Liamis

Authors
  1. V. Couaillier
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  2. R. Grenon
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  3. N. Liamis
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Editor information

M. Napolitano F. Sabetta

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© 1993 Springer-Verlag

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Couaillier, V., Grenon, R., Liamis, N. (1993). Transonic and supersonic flow calculations around aircrafts using a multidomain Euler code. 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_218

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  • DOI: https://doi.org/10.1007/3-540-56394-6_218

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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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