A comparative analysis of various shaped film-cooling holes-Reference-Cited by-同舟云学术

A comparative analysis of various shaped film-cooling holes

Published:2012-07-01 Issue:11 Volume:48 Page:1929-1939
ISSN:0947-7411
Container-title:Heat and Mass Transfer
language:en
Short-container-title:Heat Mass Transfer

Author:

Kim Sun-Min,Lee Ki-Don,Kim Kwang-Yong

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,Condensed Matter Physics

Link

http://link.springer.com/content/pdf/10.1007/s00231-012-1043-5.pdf

Reference19 articles.

1. Bunker RS (2005) A review of shaped hole turbine film-cooling technology. J Heat Transfer 127:441–453

2. Heidmann JD (2008) A numerical study of anti-vortex film cooling designs at high blowing ratio. Proceedings of the ASME Turbo Expo 2008, Berlin, GT2008-50845

3. Taslim ME (2004) Discharge coefficient measurements for flow through compound-angle conical holes with cross-flow. Int J Rotat Mach 10(2):145–153

4. Yiping Lu (2007) Effect of hole configurations on film cooling from cylindrical inclined holes for the application to gas turbine blades. Dissertation, Louisiana State University

5. Hyams DG, Leylek JH (2000) A detailed analysis of film cooling physics: part III—streamwise injection with shaped holes. J Turbomach Trans ASME 122(1):122–132

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