Non-Axisymmetric Endwall Contouring of Front-Loaded High-Lift Low Pressure Turbines
Author:
Affiliation:
1. Air Force Research Laboratory
2. Wright State University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-2125
Reference23 articles.
1. Boundary Layer Development in the BR710 and BR715 LP Turbines—The Implementation of High-Lift and Ultra-High-Lift Concepts
2. McQuilling, M. "Design and Validation of a High-Lift Low-Pressure Turbine Blade." Ph.D. Dissertation.Wright State University, 2007
3. Parametric Optimization of Unsteady End Wall Blowing on a Highly Loaded Low-Pressure Turbine
4. Eric Lyall MM, King PI, Clark JP, Sondergaard R. Endwall Loss Reduction of High Lift Low Pressure Turbine Airfoils Using Profile Contouring-Part I: Airfoil Design. ASME. J. Turbomach. 2014;136(8).
5. Application of Nonaxisymmetric Endwall Contouring to Conventional and High-Lift Turbine Airfoils
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