Hypersonic Delta Wing Flow Calculations using a Multidomain MUSCL Euler Solver

  • Ph. Guillen
  • M. Borrel
Conference paper


Euler computation results for the test case 7.1.1 from a newly developed multidomain solver (FLU3M) based on an upwind/MUSCL numerical scheme are presented. The strong influence of the grid density for an accurate prediction of the flowfield specially in the vortex region is examined through three grid refinements.




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  1. [1]
    M. Borrel, J.L. Montagné, J. Diet, Ph. Guillen, J. Lordon: “Upwind Scheme for Supersonic Flows around Tactical Missile”; La Recherche Aérospatiale, 1988-2.Google Scholar
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    Ph. Guillen, M. Dormieux:Design of a 3D Multidomain Euler Code” International Seminar on Supercomputing, Boston (USA), October 3 - 5, 1989.Google Scholar
  3. [3]
    B. van Leer: “Flux Vector Splitting of the Euler Equations”; ICASE Report 82 - 30, 1982.Google Scholar
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    S.R. Chakravarthy: High Resolution Upwind Formulation for the Navier-Stokes Equations, VKI Lecture 1988-05.Google Scholar

Copyright information

© Springer-Verlag Berlin Heidelberg 1991

Authors and Affiliations

  • Ph. Guillen
    • 1
  • M. Borrel
    • 1
  1. 1.O.N.E.R.A.ChâtillonFrance

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