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Computational Results for Flows Over Compression Ramps

  • Werner Haase
Conference paper

Summary

Steady, hypersonic viscous flows over two-dimensional compression ramps are computed by means of a finite volume technique using a Runge-Kutta type time-stepping scheme. Results are presented based on laminar flow assumptions as well as for fully turbulent flows.

Keywords

Mach Number Flat Plate Heat Transfer Rate Pressure Coefficient Separation Zone 
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References

  1. 1.
    Jameson, A., Schmidt, W., Turkel, E., “Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Schemes”, AIAA Paper 81 - 1259 (1981).Google Scholar
  2. 2.
    Haase, W., “Viscous, Hypersonic Flows Over Compression Ramps”, in: Proceedings of the Eighth GAMM-Conference on Numerical Methods in Fluids Mechanics, (Ed. P.Wesseling), Notes on Numerical Fluid Mechanics, Vol. 29, Vieweg, 1990.Google Scholar
  3. 3.
    Stock, H.W., Haase, W. “The Determination of Turbulent Length Scales in Algebraic Turbulence Models for Attached and Slightly Separated Flows Using Navier-Stokes Methods”, AIAA-Paper 87 - 1302 (1987).Google Scholar
  4. 4.
    Delery J., Coet, M.-C., “Experimental Investigations of Shock-Wave Boundary-Layer Interaction in Hypersonic Flows”, Proceedings of: Workshop on Hypersonic Flows for Reentry Problems, Vol.3, Jan. 22–25, 1990, Antibes.Google Scholar
  5. 5.
    Simeonides, G., Wendt, J.F., “Flow over a 2-D Ramp”, Proceedings of: Workshop on Hypersonic Flows for Reentry Problems, Vol.3, Jan. 22–25, 1990, AGoogle Scholar

Copyright information

© Springer-Verlag Berlin Heidelberg 1991

Authors and Affiliations

  • Werner Haase
    • 1
  1. 1.Dornier Luftfahrt GmbHFriedrichshafen 1Germany

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