Investigation of Low-Pressure Turbine Separation Control-Reference-Cited by-同舟云学术

Investigation of Low-Pressure Turbine Separation Control

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Gross Andreas¹,Fasel Hermann¹

Affiliation:

1. University of Arizona

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-520

Reference29 articles.

1. Numerical Investigation of Low-Pressure Turbine Blade Separation Control

2. 2Postl, D. “Numerical Investigation of Laminar Separation Control Using Vortex Generator Jets,” PhD dissertation,University of Arizona, Tucson, 2005

3. 4Abdessemed, N., Sherwin, S.J., and Theofilis, V. “On Unstable 2D Basic States in Low Pressure Turbine Flows at Moderate Reynolds Numbers,” AIAA-2004-2541, June-July 2004

4. Designing Low-Pressure Turbine Blades With Integrated Flow Control

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