Conjugate Heat Transfer Validation of Gas Turbine Engine Cooling Turbine Vanes

Author:

Gorelov Yu. G.

Publisher

Allerton Press

Subject

Aerospace Engineering

Reference8 articles.

1. Gorelov, Yu.G., Gorelova, D.V., Smirnova, M.A., and Berezin, A.M., Bundled Software for Analysis Thermal-Hydraulic Performances of GTE, GTU Turbine Cooling System in the Unsteady Setting, Tezisy dokladov 12-i Vseros. mezhvuzovskoi nauchno-tekhnicheskoi konf., posvyashchennoi 175-letiyu MGTU im. N.E. Baumana (Theses of Reports of the All-Russian Interuniversity Scientific and Technical Conference dedicated to the 175th Anniversary of the Moscow State Technical University named after N.E. Bauman), Moscow: MGTU im. Baumana, 2004, pp. 107–108.

2. Kassab, A., Divo, E., Heidmann, J., Steinthorsson, E., and Rodriguez, F., BEM/FVM Conjugate Heat Transfer Analysis of a Three-Dimensional Film Cooled Turbine Blade, Int. Journal of Numerical Methods for Heat and Fluid Flow, 2003, vol. 13, issue 5, pp. 581–610.

3. Heidmann, J., Kassab, A., Divo, E., Rodriguez, F., and Steinthorsson, E., Conjugate Heat Transfer Effects on a Realistic Film Cooled Turbine Vane, Proc. of the ASME Turbo Expo, 2003, Atlanta, Georgia, USA, ASME Paper no. GT2003-38553.

4. Winchler, L., Andreini, A., Facchini, B., Andrei, L., Bonini, A., and Innocenti, L., Conjugate Heat Transfer Methodology for Thermal Design and Verification of Gas Turbine Cooled Components, Journal of Turbomachinery, 2018, vol. 140, issue 12, Article no. 121001.

5. Cunliang Liu, Fan Zhang, Shuaiqi Zhang, Qingqing Shi, Hui Song, Experimental Investigation of the Full Coverage Film Cooling Effectiveness of a Turbine Blade with Shaped Holes, Chinese Journal of Aeronautics, 2022, vol. 35, issue 3, pp. 297–308.

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