Investigation of Losses on a Highly Loaded Low Pressure Turbine Blade with Unsteady Wakes-Reference-Cited by-同舟云学术

Investigation of Losses on a Highly Loaded Low Pressure Turbine Blade with Unsteady Wakes

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
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Author:

Nessler Chase¹,Marks Christopher¹,Sondergaard Rolf¹,Wolff Mitch¹

Affiliation:

1. U.S. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-302

Reference15 articles.

1. Sharma,O.,1998,"ImpactofReynoldsNumberon LPTurbinePerformance,"Proceedingsof1997 MinnowbrookIIWorkshopon BoundaryLayerTransitionin Turbomachines,NASA/CP-1998-206958.

2. High Lift and Aft-Loaded Profiles for Low-Pressure Turbines

3. Separated Flow Transition Under Simulated Low-Pressure Turbine Airfoil Conditions—Part 1: Mean Flow and Turbulence Statistics

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