A new cooling design for rib roughened two-pass channel having positive effects of rotation on heat transfer enhancement on both pressure and suction side internal walls of a gas turbine blade-Reference-Cited by-同舟云学术

A new cooling design for rib roughened two-pass channel having positive effects of rotation on heat transfer enhancement on both pressure and suction side internal walls of a gas turbine blade

Published:2017-12 Issue: Volume:115 Page:6-20
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:

Singh Prashant,Li Weihong,Ekkad Srinath V.,Ren Jing

Publisher

Elsevier BV

Subject

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

Reference33 articles.

1. Fundamental gas turbine heat transfer;Han;J. Thermal Sci. Eng. Appl.,2013

2. Gas turbine heat transfer and cooling technology;Han,2012

3. Heat transfer in rotating serpentine passages with trips skewed to the flow;Johnson;J. Turbomachinery,1994

4. Heat transfer in rotating serpentine passages with selected model orientations for smooth or skewed trip walls;Johnson;J. Turbomachinery,1994

5. Effect of rotation on heat transfer in two-pass square channels with five different orientations of 45 angled rib turbulators;Al-Hadhrami;Int. J. Heat and Mass Transf.,2003

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