Experimental Investigation of a High-Lift Low-Pressure Turbine Suction Surface
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.37579
Reference15 articles.
1. Predicting Transition in Turbomachinery—Part I: A Review and New Model Development
2. McQuilling, M. "Design and Validation of a High-Lift Low-Pressure Turbine Blade," Ph.D. Dissertation,Wright State Univ., Dayton, OH, Aug. 2007.
3. Fonov, S., Goss, L., Jones, G., Crafton, J., Fonov, V., and Ol, M. "New Method for Surface Pressure Measurements," AIAA Paper 2005-1029.
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