Augmented cooling performance in gas turbine blade tip with slot cooling-Reference-Cited by-同舟云学术

Augmented cooling performance in gas turbine blade tip with slot cooling

Published:2023-02 Issue: Volume:201 Page:123664
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:

Bang Minho^ORCID,Choi Seungyeong^ORCID,Choi Seok Min,Rhee Dong-Ho,Moon Hee Koo^ORCID,Cho Hyung Hee^ORCID

Funder

Ministry of Trade, Industry and Energy

Korea Institute of Energy Technology Evaluation and Planning

Publisher

Elsevier BV

Subject

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

Reference46 articles.

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2. E.E. Halila, D.T. Lenahan, T.T. Thomas. “Energy efficient engine high pressure turbine test hardware detailed design report (No. NASA-CR-167955).” (1982).

3. Heat transfer and pressure distributions on a gas turbine blade tip;Azad;J. Turbomach.,2000

4. Heat transfer and flow on the squealer tip of a gas turbine blade;Azad;J. Turbomach.,2000

5. Heat transfer and aerodynamics of turbine blade tips in a linear cascade;Newton;J. Turbomach.,2006

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