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Film cooling performance of blade pressure side with three-row film holes under rotating condition

  • Published:2022-06 Issue: Volume:188 Page:122593
  • 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:

Meng Long,Li Haiwang,Xie Gang,Tao Zhi,Zhou Zhiyu

Funder

National Natural Science Foundation of China

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

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

Reference40 articles.

1. Gas Turbine Heat Transfer and Cooling Technology;Han,2012

2. Gas Turbine Film Cooling;Bogard;J. Propuls. Power.,2012

3. Recent advances in film cooling enhancement: a review;Zhang;Chin. J. Aeronaut.,2020

4. Effects of hole geometry and density on three-dimensional film cooling;Goldstein;Int. J. Heat Mass Transf.,1974

5. Multi-objective optimization of round-to-slot film cooling holes on a flat surface;Huang;Aerosp. Sci. Technol.,2020
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