10.2514/1.B39899">
 

Quantification of Heat Loads in Rotating Detonation Combustors for Gas Turbines

Document Type

Article

Publication Date

1-2026

Comments

Copyright © 2025 by the American Institute of Aeronautics and Astronautics, Inc.

Source Publication

Journal of Propulsion and Power (ISSN 0748-4658 |eISSN 1533-3876)

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