Effects of Ozone Addition on Multi-Wave Modes of Hydrogen–Air Rotating Detonations
Author:
Affiliation:
1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
2. SKLTCS, CAPT, Department of Mechanics and Engineering Science, College of Engineering, Peking University, Beijing 100871, China
Abstract
Funder
National Natural Science Foundation of China
Publisher
MDPI AG
Subject
Aerospace Engineering
Link
https://www.mdpi.com/2226-4310/10/5/443/pdf
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3. Propulsion performance of cylindrical rotating detonation engine;Yokoo;AIAA J.,2020
4. Visual experimental investigation on initiation process of H2/air rotating detonation wave in plane-radial structure;Xia;Int. J. Hydrog. Energy,2020
5. Meng, Q., Zhao, N., and Zhang, H. (2021). On the distributions of fuel droplets and in situ vapor in rotating detonation combustion with prevaporized n-heptane sprays. Phys. Fluids, 33.
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2. Effects of Injector Configuration on the Detonation Characteristics and Propulsion Performance of Rotating Detonation Engine (RDE);Aerospace;2023-11-08
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