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Effects of the swirling coolant jet from the upstream slot on the vane endwall cooling and the vane suction side phantom cooling

  • Published:2018-06 Issue: Volume:121 Page:952-966
  • ISSN:0017-9310
  • Container-title:International Journal of Heat and Mass Transfer
  • language:en
  • Short-container-title:International Journal of Heat and Mass Transfer

Author:

Du Kun,Li Zhigang,Li Jun,Sunden Bengt

Funder

China Scholarship Council

National Natural Science Foundation

Swedish Research Council

Swedish National Energy Agency

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference25 articles.

1. S. Hada, K.A. Thole, Computational study of a midpassage gap and upstream slot on vane endwall film cooling, ASME Paper No. GT-2006-91067, 2006.

2. Gas Turbine Heat Transfer and Cooling Technology;Han,2000

3. Turbine endwall aerodynamics and heat transfer;Simon;AIAA J.,2006

4. A review of shaped hole turbine film-cooling technology;Bunker;ASME J. Heat Transfer.,2005

5. Fanshaped hole effects on the aero-thermal performance of a film cooled endwall;Barigozzi;ASME J. Turbomach.,2005

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1. Numerical study on film cooling effectiveness from spiral-channel hole;International Communications in Heat and Mass Transfer;2023-04

2. Research on the flow field and film cooling effectiveness of the endwall with swirling film cooling;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-05-11

3. An experimental investigation on the effects of a slot exit protrusion on film cooling effectiveness;International Journal of Thermal Sciences;2022-02

4. Effect of leakage flow on the endwall cooling performance in high subsonic turbine cascade;International Journal of Thermal Sciences;2021-12

5. Research on the effect of the swirling coolant within endwall passage on film cooling/heat transfer and aerodynamic losses;International Communications in Heat and Mass Transfer;2021-11
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