Numerical analysis for a novel cooling protection scheme with rail crown holes and streamwise divider wall for the squealer tip in a turbine blade-Reference-Cited by-同舟云学术

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Numerical analysis for a novel cooling protection scheme with rail crown holes and streamwise divider wall for the squealer tip in a turbine blade

Published:2024-09 Issue: Volume:157 Page:107815
ISSN:0735-1933
Container-title:International Communications in Heat and Mass Transfer
language:en
Short-container-title:International Communications in Heat and Mass Transfer

Author:

Zhou Haimeng,Luo Lei,Yan Han,Du Wei,Wang Songtao

Publisher

Elsevier BV

Reference41 articles.

1. Numerical evaluation of a new impingement cooling scheme with a separate return-channel applied to turbine blade leading edge;Yan;Appl. Therm. Eng.,2023

2. A critical review on gas turbine cooling performance and failure analysis of turbine blades;Chowdhury;Int. J. Thermofluids,2023

3. A review of recent studies on rotating internal cooling for gas turbine blades;Yeranee;Chin. J. Aeronaut.,2021

4. Effect of turbine blade tip cooling configuration on tip leakage flow and heat transfer;Sakaoglu;J. Turbomach.,2020

5. The impact of mainstream ingress on the leakage flow and loss in partial shrouded turbines;Zhang;Aerosp. Sci. Technol.,2023

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