Operational mode transition in a rotating detonation engine-Reference-Cited by-同舟云学术

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Operational mode transition in a rotating detonation engine

Published:2020-09 Issue:9 Volume:21 Page:721-733
ISSN:1673-565X
Container-title:Journal of Zhejiang University-SCIENCE A
language:en
Short-container-title:J. Zhejiang Univ. Sci. A

Author:

Lei Zhi-di^ORCID,Chen Zheng-wu,Yang Xiao-quan,Ding Jue,Weng Pei-fen

Funder

National Natural Science Foundation of China

the Open Project Program of the Key Laboratory of Aerodynamic Noise Control of China Aerodynamics Research and Development Center

the CARDC Fundamental and Frontier Technology Research Fund

the Open Project Program of Rotor Aerodynamics Key Laboratory , China

Publisher

Zhejiang University Press

Subject

General Engineering

Link

https://link.springer.com/content/pdf/10.1631/jzus.A1900349.pdf

Reference37 articles.

1. Anand V, George AS, Driscoll R, et al., 2015. Characterization of instabilities in a rotating detonation combustor. International Journal of Hydrogen Energy, 40(46):16649–16659. https://doi.org/10.1016/j.ijhydene.2015.09.046

2. Anand V, George AS, Driscoll R, et al., 2016. Investigation of rotating detonation combustor operation with H2-air mixtures. International Journal of Hydrogen Energy, 41(2):1281–1292. https://doi.org/10.1016/j.ijhydene.2015.11.041

3. Bader G, Deuflhard P, 1983. A semi-implicit mid-point rule for stiff systems of ordinary differential equations. Numerische Mathematik, 41(3):373–398. https://doi.org/10.1007/BF01418331

4. Bykovskii FA, Vedernikov EF, 1996. Self-sustaining pulsating detonation of gas-mixture flow. Combustion, Explosion and Shock Waves, 32(4):442–448. https://doi.org/10.1007/BF01998496

5. Bykovskii FA, Zhdan SA, Vedernikov EF, 2005. Continuous spin detonation in annular combustors. Combustion, Explosion and Shock Waves, 41(4):449–459. https://doi.org/10.1007/s10573-005-0055-6

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3. An Investigation on the Wave Multiplicity and Control of Operating Modes in the Hydrogen-Fueled Rotating Detonation Engine;2023

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