Boundary Layer Instabilities in Transonic Range of Velocities

Autor:	Oleg S. Ryzhov, Elena V. Bogdanova-Ryzhova
Rok vydání:	2003
Předmět:	Physics Turbine blade Wave packet Reynolds number Mechanics law.invention Vortex Physics::Fluid Dynamics symbols.namesake Boundary layer Mach number law symbols Swept wing Transonic Astrophysics::Galaxy Astrophysics
Zdroj:	IUTAM Symposium Transsonicum IV ISBN: 9789401039987
DOI:	10.1007/978-94-010-0017-8_19
Popis:	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 Gortier vortices on a concave surface and vortical disturbances in a three-dimensional boundary layer with crossflow on a swept wing or turbine blade.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::c448b1aaaf24d604e1f3399d2d4f55eb https://doi.org/10.1007/978-94-010-0017-8_19 Zobrazit plný text záznamu