Numerical Investigation of Plasma-Based Flow Control for Transitional Highly-Loaded Low-Pressure Turbine
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433-7512
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.29602
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1. Reducing Low-Pressure Turbine Stage Blade Count Using Vortex Generator Jet Separation Control
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