Numerical Investigation of Active Flow Control for Front-Loaded Low-Pressure Turbine Cascade
Author:
Affiliation:
1. New Mexico State University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1832
Reference37 articles.
1. BLADEROW INTERACTIONS, TRANSITION, AND HIGH-LIFT AEROFOILS IN LOW-PRESSURE TURBINES
2. Boundary Layer Development in the BR710 and BR715 LP Turbines—The Implementation of High-Lift and Ultra-High-Lift Concepts
3. 3McQuilling, M.W. “Design and Validation of a High-Lift Low-Pressure Turbine Blade,” PhD Thesis,Wright State University, Dayton, OH, 2007.
4. Secondary Flows and Losses Downstream of a Turbine Cascade
5. Growth of Secondary Losses and Vorticity in an Axial Turbine Cascade
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3. Numerical Investigation of Active Flow Control of Low-Pressure Turbine Endwall Flow;Journal of Propulsion and Power;2019-09
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