A numerical study of the effect of wake passing on turbine blade film cooling-Reference-Cited by-同舟云学术

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A numerical study of the effect of wake passing on turbine blade film cooling

Published:1995-07-10 Issue: Volume: Page:
ISSN:
Container-title:31st Joint Propulsion Conference and Exhibit
language:
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Author:

Heidmann James

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-3044

Reference14 articles.

1. The 1991 IGTI Scholar Lecture: The Role of Laminar-Turbulent Transition in Gas Turbine Engines

2. Eckert,E. R. G., etal,"Studiesof GasTurbine Heat Transfer: Airfoil SurfacesandEnd-Wall Cooling Efl'ccts",AirForce Officeof ScientificResearch, ReportN92-19097, Sept. 1991

3. W Transferin Rotor/StatorInterming Flows", N00140-88-C-0677 -RcportI.UTRCRcport 91-29, Apr. 1992.

Cited by 2 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. Convective Heat Transfer and Aerodynamics in Axial Flow Turbines;Journal of Turbomachinery;2001-02-01

2. An Experimental Study of the Effect of Wake Passing on Turbine Blade Film Cooling;Journal of Turbomachinery;1997-02-01

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