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Boundary Layer Instabilities in Transonic Range of Velocities

  • Oleg S. Ryzhov
  • Elena V. Bogdanova-Ryzhova
Part of the Fluid Mechanics and its Applications book series (FMIA, volume 73)

Abstract

An extended version of the triple-deck theory is developed for high Mach number subsonic and transonic flows, assuming the Reynolds number to be large enough. The theory embraces unsteady spiral-type Görtier vortices on a concave surface and vortical disturbances in a three-dimensional boundary layer with crossflow on a swept wing or turbine blade.

Keywords

Wave Packet Dispersion Curve Transonic Flow Side Band Absolute Instability 
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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Copyright information

© Springer Science+Business Media Dordrecht 2003

Authors and Affiliations

  • Oleg S. Ryzhov
    • 1
  • Elena V. Bogdanova-Ryzhova
    • 2
  1. 1.Department of Mechanical and Aeronautical EngineeringUniversity of California DavisDavisUSA
  2. 2.GE Global ResearchFluid Mechanics LaboratorySchenectadyUSA

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