Computational fluid dynamics evaluations of unconventional film cooling scaling parameters on a simulated turbine blade leading edge

Authors

• James L. Rutledge, Air Force Institute of TechnologyFollow
• Marc D. Polanka, Air Force Institute of TechnologyFollow

Document Type

Article

Publication Date

10-2014

Comments

Copyright © 2014 by ASME

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

Paper No: TURBO-14-1018

DOI

10.1115/1.4028001

Source Publication

Journal of Turbomachinery (ISSN 0889-504X | eISSN 1528-8900)

Recommended Citation

Rutledge, J. L., and Polanka, M. D. (July 29, 2014). "Computational Fluid Dynamics Evaluations of Unconventional Film Cooling Scaling Parameters on a Simulated Turbine Blade Leading Edge." ASME. J. Turbomach. October 2014; 136(10): 101006. https://doi.org/10.1115/1.4028001