Effects of pressure side film cooling hole placement and condition on adiabatic film cooling effectiveness characteristics of a transonic turbine blade tip-Reference-Cited by-同舟云学术

Effects of pressure side film cooling hole placement and condition on adiabatic film cooling effectiveness characteristics of a transonic turbine blade tip

Published:2022-12 Issue: Volume:199 Page:123462
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:

Collopy Hallie^ORCID,Ligrani Phillip M.,Xu Hongzhou,Fox Michael^ORCID

Publisher

Elsevier BV

Subject

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

Reference21 articles.

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4. Turbine blade tip heat transfer in low speed and high speed flows;Wheeler;J. Turbomach.,2011

5. Overtip shock wave structure and its impact on turbine blade tip heat transfer;Zhang;J. Turbomach.,2011

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