Numerical investigation on the effect of rotation on impingement cooling of the gas turbine leading edge
Author:
Funder
United Arab Emirates University
Publisher
Elsevier BV
Subject
General Engineering
Reference21 articles.
1. Experimental and numerical investigation of impingement on a rib-roughened leading-edge wall;Taslim;J. Turbomach.,2003
2. Z. Liu, Z. Feng, L. Song, Numerical study on flow and heat transfer characteristics of swirl cooling on leading edge model of gas turbine blade no. 54655, 2011, pp. 1495–1504. https://doi.org/10.1115/GT2011-46125.
3. Local heat transfer in internally cooled turbine airfoil leading edge regions: Part I—Impingement cooling without film coolant extraction;Bunker;J. Turbomach.,1990
4. Numerical simulation on the effect of jet nozzle position on impingement cooling of gas turbine blade leading edge;Liu;Int. J. Heat Mass Transf.,2011
5. Measurement and modeling of confined jet discharged tangentially on a concave semi-cylindrical hot surface;Hamdan;J. Heat Transf.,2011
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