Reynolds Stress Transport Modeling of Film Cooling at the Leading Edge of a Symmetrical Turbine Blade Model-Reference-Cited by-同舟云学术

Reynolds Stress Transport Modeling of Film Cooling at the Leading Edge of a Symmetrical Turbine Blade Model

Published:2008-11 Issue:11 Volume:29 Page:950-960
ISSN:0145-7632
Container-title:Heat Transfer Engineering
language:en
Short-container-title:Heat Transfer Engineering

Author:

Nemdili Fadéla,Azzi Abbès,Theodoridis Georgios,Jubran Bassam A.

Publisher

Informa UK Limited

Subject

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

Link

http://www.tandfonline.com/doi/pdf/10.1080/01457630802186064

Reference21 articles.

1. The Near-Field Character of a Jet Discharged Normal to a Main Stream

2. Experimental investigation of jets in a crossflow

3. Gas Turbine Film Cooling

4. A Review of Shaped Hole Turbine Film-Cooling Technology

5. Haslinger, W. and Hennecke, D. K. 1997. High Resolved Distribution of Adiabatic Film Cooling Effectiveness for Turbine Leading Edge Film Cooling. Proc. 13th Int. Symposium Air Breathing Engines. Sept.1997, Chattanooga, Tenn. pp.797–806. ISABE 97–7113

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