Characteristic velocity analysis of the total pressure gain of rotating detonation combustors-Reference-Cited by-同舟云学术

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Characteristic velocity analysis of the total pressure gain of rotating detonation combustors

Published:2024 Issue:1-4 Volume:40 Page:105626
ISSN:1540-7489
Container-title:Proceedings of the Combustion Institute
language:en
Short-container-title:Proceedings of the Combustion Institute

Author:

Jiao Zhongtian,Wang Ke^ORCID,Xiao Qiang,Zhang Yonghui^ORCID,Fan Wei

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference31 articles.

1. Effects of cavity location on ethylene–air continuous rotating detonation in a cavity-based annular combustor;Peng;Combust. Sci. Technol.,2021

2. Continuous detonation combustion of fuel-air mixtures;Bykovskii;Combust., Explos. Shock Waves.,1997

3. T.A. Kaemming, D.E. Paxson, Determining the pressure gain of pressure gain combustion, AIAA Paper 2018-4567, 2018.

4. D. Schwer, K. Kailasanath, Feedback into mixture plenums in rotating detonation engines, AIAA Paper 2012-617, 2012.

5. Theoretical and numerical investigation on total pressure gain in rotating detonation engine;Zhang;AIAA J,2020

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