Numerical Study of Heat Transfer in a Rotating Detonation Combustor-Reference-Cited by-同舟云学术

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Numerical Study of Heat Transfer in a Rotating Detonation Combustor

Published:2015-01-03 Issue: Volume: Page:
ISSN:
Container-title:53rd AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Randall Steven¹,Anand Vijay¹,St. George Andrew C.¹,Gutmark Ephraim J.¹

Affiliation:

1. University of Cincinnati

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0880

Reference33 articles.

1. Experimental Comparison of Axial Turbine Performance Under Steady and Pulsating Flows

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1. Experimental Investigation of Thermal Prediction and Heat Transfer Characteristics of Two-Phase RDE during Long-Duration Operation;Energies;2024-05-27

2. Comprehensive analysis method of acquiring wall heat fluxes in rotating detonation combustors;Experimental Thermal and Fluid Science;2024-03

3. Exploring critical detonation parameters in Ethylene-oxygen detonations;AIP Conference Proceedings;2023

4. CALCULATION OF THE HEAT TRANSFER COEFFICIENT IN THE OUTER BODY FOR A ROTATIONAL DETONATION ENGINE;International Journal of Energy for a Clean Environment;2023

5. Using Ozone and Hydrogen Peroxide for Manipulating the Velocity Deficits, Detonabilility, and Flammability Limits of Gaseous Detonations;Proceedings of the National Aerospace Propulsion Conference;2022-07-24

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