LES-based investigation on external heat transfer characteristics of turbine blades for gas turbine (About the effect of turbine blades configuration)
Author:
Affiliation:
1. Kawasaki Heavy Industries, LTD. Thermal System Research Dept. Technical Institute
2. Iwate University Department of Mechanical Engineering.
Publisher
Japan Society of Mechanical Engineers
Link
https://www.jstage.jst.go.jp/article/transjsme/81/822/81_14-00420/_pdf
Reference13 articles.
1. Arts, T., Duboue, J. and Rollin, G., Aero-thermal performance measurements and analysis of two-dimensional high turning rotor blade, International Gas Turbine & Aero engine Congless & Exhibition (1997).
2. Dyson,T. E., Bogard, D. G. and Bradshaw, S. D., A CFD evaluation of multiple RANS turbulence models for prediction of boundary layer flows on a turbine vane, ASME Turbo Expo(2013), GT2013-94927.
3. FLUENT theory guide, ANSYS Inc, (2010) (in Japanese).
4. Gourdain, N., Duchaine, F. and Collado, E., Advanced numerical simulation dedicated to the prediction of heat transfer in a highly loaded turbine guide vane, ASME Turbo Expo(2010), GT2010-22793.
5. Kobayashi,K., Taniguchi,N. and Kobayashi,T., Construction of LES wall model by using zero equation RANS models(validation in channel flow) (in Japanese).
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