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A direct method for computing the steady flow at mach number one past a given wing airfoil

  • D. Euvrard
  • G. Tournemine
Conference paper
Part of the Lecture Notes in Physics book series (LNP, volume 19)

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References

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    D. Euvrard, G. Tournemine, C.R. Acad. Sc. Paris, t. 274, série A, 27 mars 1972, pp. 1071–1074.Google Scholar
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Copyright information

© Springer-Verlag 1973

Authors and Affiliations

  • D. Euvrard
    • 1
  • G. Tournemine
    • 1
  1. 1.Département de Mathématiques et InformatiqueUniversité de RennesFrance

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