Periodic Forcing of an Endwall Vortex in a Highly Loaded Low Pressure Turbine

Author:

Donovan Molly H.1,Wolff Mitch1,Marks Christopher R.2,Sondergaard Rolf2,Veley Emma2

Affiliation:

1. Wright State University

2. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Reference20 articles.

1. Development of Blade Profiles for Low-Pressure Turbine Applications

2. Clark, J. P., Koch, P. J., Puterbaugh, S. L. Schmitz, J. T., Morris, S. C., Ma, R., and Corke, T. C. "Highly Loaded Low-Pressure Turbine: Design, Numerical and Experimental Analysis," AFRL Report: AFRL-RZ-WP-TP-2010-2143.

3. McQuilling, M. W. "Design and Validation of a High-Lift Low-Pressure Turbine Blade," Ph.D. Dissertation,Wright State University, 2007.

4. Time-depeiident and time-averaged turbulence structure near the nose of a wing-body junction

5. Experimental Investigation of Total Pressure Loss Development in a Highly Loaded Low-Pressure Turbine Cascade

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