Numerical Study of Active Flow Control for a Transitional Highly-Loaded Low-Pressure Turbine-Reference-Cited by-同舟云学术

Numerical Study of Active Flow Control for a Transitional Highly-Loaded Low-Pressure Turbine

Published:2005-06-06 Issue: Volume: Page:
ISSN:
Container-title:35th AIAA Fluid Dynamics Conference and Exhibit
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Author:

Rizzetta Donald¹,Visbal Miguel¹

Affiliation:

1. U.S. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-5020

Reference53 articles.

1. Boundary Layer Development in Axial Compressors and Turbines: Part 1 of 4 — Composite Picture

2. Boundary Layer Development in Axial Compressors and Turbines: Part 3 of 4 — LP Turbines

3. 4Baughn, J. W., Butler, R. J., Byerley, A. R., and Rivir, R. B. “An Experimental Investigation of Heat Transfer, Transition and Separation on Turbine Blades at Low Reynolds Number and High Turbulence Intensity,” Technical Report WL-TR-96-2093, Wright Laboratory, Wright-Patterson AFB, OH, Jul. 1996.

4. Experimental Study of the Unsteady Aerodynamics in a Linear Cascade With Low Reynolds Number Low Pressure Turbine Blades

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