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Hypersonic Shock-Wave/Boundary Layer Interactions with an Implicit Navier-Stokes Solver

  • Pénélope Leyland
Conference paper

Abstract

A fully implicit Navier-Stokes solver is used to calculate two-dimensionnal generic hypersonic geometries. Peak heating and shock wave/boundary layer interaction features are illustrated by computations over compression ramps, (representative of flows over control surfaces), and generic nose-to-canopy flows (double ellipse geometry with zero incident flow). Comparisons with experimental data is commented.

Key words

Boundary-layer interactions Separation Reattachment Hypersonics 

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References

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Copyright information

© Springer-Verlag Berlin Heidelberg 1995

Authors and Affiliations

  • Pénélope Leyland
    • 1
  1. 1.Institut de Machines Hydrauliques et Mécanique des FluidesEcole Polytechnique Fédérale de LausanneLausanneSwitzerland

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