Film cooling parameter waveforms on a turbine blade leading edge model with oscillating stagnation line

Authors

• James L. Rutledge, Air Force Institute of TechnologyFollow
• Tylor C. Rathsack, Air Force Institute of Technology
• Matthew T. Van Voorhis, Air Force Institute of Technology
• Marc D. Polanka, Air Force Institute of TechnologyFollow

Document Type

Article

Publication Date

7-2016

Comments

Copyright © 2016 by ASME

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

Paper No: TURBO-15-1287

DOI

10.1115/1.4032455

Source Publication

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

Recommended Citation

Rutledge, J. L., Rathsack, T. C., Van Voorhis, M. T., and Polanka, M. D. (February 17, 2016). "Film Cooling Parameter Waveforms on a Turbine Blade Leading Edge Model With Oscillating Stagnation Line." ASME. J. Turbomach. July 2016; 138(7): 071005. https://doi.org/10.1115/1.4032455