The effect of dimple/protrusion arrangements on the comprehensive thermal performance of variable cross-section rotating channels for gas turbine blades-Reference-Cited by-同舟云学术

The effect of dimple/protrusion arrangements on the comprehensive thermal performance of variable cross-section rotating channels for gas turbine blades

Published:2024-02 Issue: Volume:196 Page:108733
ISSN:1290-0729
Container-title:International Journal of Thermal Sciences
language:en
Short-container-title:International Journal of Thermal Sciences

Author:

Shi Dongbo^ORCID,Xu Tao,Chen Zifeng^ORCID,Zhang Di,Xie Yonghui

Funder

Fundamental Research Funds for the Central Universities

National Major Science and Technology Projects of China

Publisher

Elsevier BV

Subject

General Engineering,Condensed Matter Physics

Reference39 articles.

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2. Gas Turbine Heat Transfer and Cooling technology[M]. Xi'an;Cheng,2007

3. Development status and prospect of aviation material technology;Yan;Aviation Manuf. Technol.,2003

4. Study on advanced internal cooling technologies for the development of next-generation small-class aircraft engines;Fujimoto;J. Turbomach.,2010

5. Effects of channel aspect ratio on heat transfer in rectangular passage sharp 180-deg turns[C];Fan,1987

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