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.
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© 2003 Springer Science+Business Media Dordrecht
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Ryzhov, O.S., Bogdanova-Ryzhova, E.V. (2003). Boundary Layer Instabilities in Transonic Range of Velocities. In: Sobieczky, H. (eds) IUTAM Symposium Transsonicum IV. Fluid Mechanics and its Applications, vol 73. Springer, Dordrecht. https://doi.org/10.1007/978-94-010-0017-8_19
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DOI: https://doi.org/10.1007/978-94-010-0017-8_19
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