Simulation of Transonic Flow through a Mid-span Turbine Blade Cascade for Various Mach Numbers

被引：1
|
作者：
Petr, Straka [1 ]
Jaromir, Prihoda [2 ]
David, Fenderl [3 ]
机构：
[1] Aerosp Test & Res Estab Plc, Beranovych 130, Prague 19905 9, Czech Republic
[2] Inst Thermomech AS CR, Vvi, Dolejskova 5, Prague 18200 8, Czech Republic
[3] Doosan Skoda Power Co Ltd, Tylova 1-57, Plzen 30128, Czech Republic
来源：
36TH MEETING OF DEPARTMENTS OF FLUID MECHANICS AND THERMODYNAMICS | 2017年 / 1889卷
关键词：
TRANSITION;
D O I：
10.1063/1.5004376
中图分类号：
O414.1 [热力学];
学科分类号：
摘要：
The contribution deals with the numerical simulation of 2D transonic flow through a mid-span turbine blade cascade for several Mach numbers by means of the EARSM turbulence model of Hellsten [1] connected with the algebraic bypass transition model of Straka and Prihoda [2]. Both models are implemented into an in-house numerical code based on the finite volume method. The gamma transition model of Menter et al. [3] with SST turbulence model accessible in the commercial code ANSYS Fluent was used for the comparison.
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页数：7
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