Numerical study on the influence of coolant temperature, pressure, and thermal barrier coating thickness on heat transfer in high-pressure blades-Reference-Cited by-同舟云学术

Numerical study on the influence of coolant temperature, pressure, and thermal barrier coating thickness on heat transfer in high-pressure blades

Published:2022-06 Issue: Volume:189 Page:122715
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:

Vo Duy-Tan,Mai Thanh Dam^ORCID,Kim Byungwook,Ryu Jaiyoung

Publisher

Elsevier BV

Subject

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

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5. Film cooling characteristics on the leading edge of a rotating turbine blade with various mainstream Reynolds numbers and coolant densities;Li;Int. J. Heat Mass Transf.,2018

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