Performance of Compound Angled Cooling Holes Within a Rotating Detonation Combustor

Authors

• Shreyas Ramanagar-Sridhara, University of Florence
• Marc D. Polanka, Air Force Institute of TechnologyFollow
• Myles D. Bohon, Technische Universitat Berlin
• Antonio Andreini, University of Florence

Document Type

Article

Publication Date

12-2026

Comments

Copyright © 2026 by ASME.

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

DOI

10.1115/1.4072583

Source Publication

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

Recommended Citation

Ramanagar-Sridhara, S., Polanka, M. D., Bohon, M. D., and Andreini, A. (September 21, 2026). "Performance of Compound Angled Cooling Holes Within a Rotating Detonation Combustor." ASME. J. Turbomach. December 2026; 148(12): 121003. https://doi.org/10.1115/1.4072583