Computational Results for 2-D and 3-D Ramp Flows with an Upwind Navier-Stokes Solver

  • Ethiraj Venkatapathy
Conference paper


An implicit, finite-difference, upwind, full Navier-Stokes solver has been applied to supersonic/hypersonic flows over two-dimensional ramps and three-dimensional obstacle (Problem sets 3 and 4). Some of the computed numerical results are presented here.




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  1. 1.
    Obayashi, S. Numerical Simulation of Underexpanded Plumes using Upwind Algorithms, AIAA Paper 88-4360-CP, 1988.Google Scholar
  2. 2.
    Venkatapathy, E., Feiereisen, W. J. and Obayashi, S.,Computational Studies of Hard Body and 3-D Effects in Plume Flows, AIAA Paper 88–3158, 1988.Google Scholar

Copyright information

© Springer-Verlag Berlin Heidelberg 1991

Authors and Affiliations

  • Ethiraj Venkatapathy
    • 1
    • 2
  1. 1.Eloret InstitutePalo AltoUSA
  2. 2.MS 230-2, ARCNASAUSA

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