Predicting Separation and Transitional Flow in Turbine Blades at Low Reynolds Numbers-Part II: The Application to a Highly Separated Turbine Blade Cascade Geometry

Authors

• Darius D. Sanders, Air Force Research Laboratory
• Walter F. O'Brien, Air Force Research Laboratory
• Rolf Sondergaard, Air Force Research Laboratory
• Marc D. Polanka, Air Force Institute of TechnologyFollow
• Douglas C. Rabe, Air Force Research Laboratory

Document Type

Article

Publication Date

7-2011

Comments

Copyright © 2011 by American Society of Mechanical Engineers

The full article is available via subscription or purchase using the DOI link below.

DOI

10.1115/1.4001231

Source Publication

Journal of Turbomachinery

Recommended Citation

Sanders, D. D., O’Brien, W. F., Sondergaard, R., Polanka, M. D., and Rabe, D. C. (November 15, 2010). "Predicting Separation and Transitional Flow in Turbine Blades at Low Reynolds Numbers—Part II: The Application to a Highly Separated Turbine Blade Cascade Geometry." ASME. J. Turbomach. July 2011; 133(3): 031012. https://doi.org/10.1115/1.4001231