Superposition of Overall Cooling Effectiveness on a Turbine Blade Leading Edge

Authors

Bailey Hopkins, Air Force Research Laboratory
James L. Rutledge, Air Force Institute of TechnologyFollow

Document Type

Article

Publication Date

2-28-2025

Comments

This article was published by ASME in February 2025 online as an article of Journal of Turbomachinery, ahead of inclusion in the October 2025 issue.

ASME Paper No: TURBO-24-1173

DOI

10.1115/1.4067886

Source Publication

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

Recommended Citation

Hopkins, B. W., and Rutledge, J. L. (February 28, 2025). "Superposition of Overall Cooling Effectiveness on a Turbine Blade Leading Edge." ASME. J. Turbomach. October 2025; 147(10): 101001. https://doi.org/10.1115/1.4067886