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Matematical Modeling of Supersonic Turbulent Flows in Inlets with Rotating Cowl

  • Bedarev I. A. 
  • Fedorova N. N. 
  • Goldfeld M. A. 
  • Falempin F. 

Keywords

Shock Wave Mach Number Blow Down Boundary Layer Interaction Compute Pressure 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

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    Bourdeau C., Blaize M. and Knight D.: AIAA Paper 99-0611.Google Scholar
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    Falempin F., Goldfeld M., Nestoulia R., Starov A.: AIAA Paper No 2002-5232.Google Scholar
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    Borisov A.V., Fedorova N.N.: Thermophisics and Aeromechanics, 4,1, pp. 69–83 (1996).Google Scholar
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    Bedarev I.A., Borisov A.V., Fedorova N.N.: Comp. Fluid Dyn. Journ., 10, Special Number, pp. 194–202 (2001).Google Scholar
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    Fedorova N.N., Fedorchenko I.A., Shuelein E.: Comp. Fluid Dyn. Journ. 10,3, pp. 376–381 (2001).Google Scholar
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    Bedarev I.A., Fedorova N.N.: First Int. Conf. CFD (Kyoto, Japan, 2000) pp. 343–344.Google Scholar

Copyright information

© Springer-Verlag Berlin Heidelberg 2006

Authors and Affiliations

  • Bedarev I. A. 
    • 1
  • Fedorova N. N. 
    • 1
  • Goldfeld M. A. 
    • 1
  • Falempin F. 
    • 2
  1. 1.Institute of Theoretical and Applied MechanicsNovosibirskRussia
  2. 2.MBDAChatillonFrance

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