Conjugate heat transfer of a rib-roughened internal turbine blade cooling channel using large eddy simulation-Reference-Cited by-同舟云学术

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Conjugate heat transfer of a rib-roughened internal turbine blade cooling channel using large eddy simulation

Published:2016-10 Issue: Volume:61 Page:650-664
ISSN:0142-727X
Container-title:International Journal of Heat and Fluid Flow
language:en
Short-container-title:International Journal of Heat and Fluid Flow

Author:

Scholl Sebastian^ORCID,Verstraete Tom,Duchaine Florent,Gicquel Laurent

Publisher

Elsevier BV

Subject

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

Reference59 articles.

1. Conjugate heat transfer investigation of rib-roughened cooling channels;Agostini,2005

2. A study of rotor cavities and heat transfer in a cooling process in a gas turbine;Amano;ASME J. Turbomach,1994

3. Experimental and numerical investigation of flow and heat transfer in a ribbed duct;Arts,2007

4. Aero-Thermal Investigation of Fixed Rib-Roughened Cooling Passages;Cakan,2000

5. Aerodynamic Performance Investigation of a Fixed Rib-Roughened Internal Cooling Passage;Casarsa,2003

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