Enhanced thermal performance of a pin-fin cooling channel for gas turbine blade by density-based topology optimization-Reference-Cited by-同舟云学术

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Enhanced thermal performance of a pin-fin cooling channel for gas turbine blade by density-based topology optimization

Published:2022-11 Issue: Volume:181 Page:107783
ISSN:1290-0729
Container-title:International Journal of Thermal Sciences
language:en
Short-container-title:International Journal of Thermal Sciences

Author:

Yeranee Kirttayoth,Rao Yu,Yang Li,Li Hao

Funder

National Natural Science Foundation of China

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

General Engineering,Condensed Matter Physics

Reference56 articles.

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

2. Multiple-jet impingement heat transfer in double-wall cooling structures with pin fins and effusion holes;Rao;Int. J. Therm. Sci.,2018

3. Flow and heat transfer characteristics in latticework cooling channels with dimple vortex generators;Rao;ASME J. Turbomach.,2014

4. Experimental and numerical study of heat transfer and turbulent flow characteristics in three-short-pass serpentine cooling channels with miniature W-ribs;Rao;J. Heat Tran.,2020

5. Heat transfer and pressure loss of turbulent flow in channels with miniature structured ribs on one wall;Li;Int. J. Heat Mass Tran.,2019

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