Home > Conference materials > Papers > Simulation of Compressible Flow Through the Tip-Section Turbine Blade Cascade with the Unsteady Interaction of the Shock wave with Shear Layers
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