Original title: Modelling of Flow in Linear Blade Cascade with Thick Trailing Edge at a Lower Reynolds Number
Authors: Straka, P. ; Příhoda, Jaromír
Document type: Papers
Conference/Event: Engineering Mechanics 2017 /23./, Svratka (CZ), 20170515
Year: 2017
Language: eng
Abstract: In the paper there are compared results of numerical simulation of compressible turbulent flow through a low-pressure turbine blade cascade with relatively thick trailing edges for various physical models. Steady, unsteady, fully turbulent, transitional, two-dimensional and three-dimensional models are compared. Results show that: a) steady simulation gives an incorrect prediction of the boundary layer development, b) two-dimensional unsteady simulation leads to inaccurate prediction of the far wake development and c) only three-dimensional unsteady transitional simulation gives sufficiently accurate prediction. Results of numerical simulations are compared with the experimental data.
Keywords: boundary layer transition; linear blade cascade; vortex series
Project no.: TA04020129 (CEP)
Funding provider: GA TA ČR
Host item entry: Engineering Mechanics 2017, ISBN 978-80-214-5497-2, ISSN 1805-8248

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/11104/0279591

Permalink: http://www.nusl.cz/ntk/nusl-371045


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Research > Institutes ASCR > Institute of Thermomechanics
Conference materials > Papers
 Record created 2018-01-11, last modified 2022-09-29


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