Original title: Simulation of Compressible Flow Through the Tip-Section Turbine Blade Cascade with the Unsteady Interaction of the Shock wave with Shear Layers
Authors: Straka, P. ; Příhoda, Jaromír ; Bobčík, M.
Document type: Papers
Conference/Event: Topical Problems of Fluid Mechanics 2016, Praha (CZ), 2016-02-10 / 2016-02-12
Year: 2016
Language: eng
Abstract: The contribution deals with the numerical simulation of compressible ow through the tip- section turbine blade cascade with the supersonic inlet boundary conditions. The simulation was carried out by the in-house numerical code using the explicit algebraic Reynolds stress model completed by the bypass transition model with the algebraic equation for the inter- mittency coefficient. The simulation was focused particularly on the shock-wave/boundary layer interaction resulting in combination of the bypass-transition and the separation induced transition.
Keywords: boundary layer transition; CFD; compressible flow; shock wave interaction; tip-section blade cascade
Project no.: TA03020277 (CEP), GAP101/12/1271 (CEP)
Funding provider: GA TA ČR, GA ČR
Host item entry: Topical Problems of Fluid Mechanics 2016, ISBN 978-80-87012-58-1
Note: Související webová stránka: http://www.it.cas.cz/fm2015/im/im/page/papers%202016

Institution: Institute of Thermomechanics AS ČR (web)
Document availability information: Fulltext is available at the institute of the Academy of Sciences.
Original record: http://hdl.handle.net/11104/0260670

Permalink: http://www.nusl.cz/ntk/nusl-253608


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Research > Institutes ASCR > Institute of Thermomechanics
Conference materials > Papers