Influence of film cooling unsteadiness on turbine blade leading edge heat flux

Authors

• James L. Rutledge, Air Force Institute of TechnologyFollow
• Paul I. King, Air Force Institute of Technology
• Richard B. Rivir, Air Force Research Laboratory

Document Type

Article

Publication Date

7-2012

Comments

Copyright © 2012 by American Society of Mechanical Engineers

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

DOI

10.1115/1.4005978

Source Publication

Journal of Engineering for Gas Turbines and Power (ISSN 0742-4795 | eISSN 1528-8919)

Recommended Citation

Rutledge, J. L., King, P. I., and Rivir, R. B. (May 23, 2012). "Influence of Film Cooling Unsteadiness on Turbine Blade Leading Edge Heat Flux." ASME. J. Eng. Gas Turbines Power. July 2012; 134(7): 071901. https://doi.org/10.1115/1.4005978