Three-dimensional Navier-Stokes heat transfer predictions for turbine blade rows-Reference-Cited by-同舟云学术

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Three-dimensional Navier-Stokes heat transfer predictions for turbine blade rows

Published:1992-07-06 Issue: Volume: Page:
ISSN:
Container-title:28th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

BOYLE R.¹,GIEL P.²

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

2. Sverdrup Technology, Inc.; NASA, Lewis Research Center, Cleveland,OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3068

Reference22 articles.

1. *An Experimental Study of Endwall and Airfoil Surfme Heat Transfer Cascade,' ASME 3.oJEnginrrring10,Power, Vol. 102, No. 2 April, 1980.

2. Film Cooling inLarge-ScaleTurbine Endwalk," ASME Jormd 01Heat 3tonsjcr.Vol 96,pp.525-529, 1974.

3. n i of Turbine Passage Heat Trader," , AlAA paper 91-2241, 1991.

Cited by 11 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Two-equation turbulence models for prediction of heat transfer on a transonic turbine blade;International Journal of Heat and Fluid Flow;2001-12

2. Modeling film-coolant flow characteristics at the exit of shower-head holes;International Journal of Heat and Fluid Flow;2001-04

3. Heat transfer on a film-cooled rotating blade;International Journal of Heat and Fluid Flow;2000-04

4. Heat transfer on a film-cooled rotating blade using different turbulence models;International Journal of Heat and Mass Transfer;1999-03

5. Heat transfer on a film-cooled blade – effect of hole physics;International Journal of Heat and Fluid Flow;1999-02

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