Affiliation:
1. New Mexico State University
Publisher
American Institute of Aeronautics and Astronautics
Reference69 articles.
1. 1McQuilling, M.W. “Design and Validation of a High Lift Low-Pressure Turbine Blade,” Ph.D. Dissertation,Wright State University, Dayton, OH, 2007
2. 2Lyall, M.E. “Effects of Front-Loading and Stagger Angle on Endwall Losses of High Lift Low Pressure Turbine Vanes,” Ph.D. Dissertation,Air Force Institute of Technology, 2012
3. The Influence of Load Distribution on Secondary Flow in Straight Turbine Cascades
4. Comparative Investigation of Three Highly Loaded LP Turbine Airfoils: Part I — Measured Profile and Secondary Losses at Design Incidence
5. Endwall Loss Reduction of High Lift Low Pressure Turbine Airfoils Using Profile Contouring—Part I: Airfoil Design