Suppression of pressure feedback of the rotating detonation combustor by a Tesla inlet configuration-Reference-Cited by-同舟云学术

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Suppression of pressure feedback of the rotating detonation combustor by a Tesla inlet configuration

Published:2022-11 Issue: Volume:216 Page:119123
ISSN:1359-4311
Container-title:Applied Thermal Engineering
language:en
Short-container-title:Applied Thermal Engineering

Author:

Yang Xingkui,Song Feilong,Wu Yun,Guo Shanguang,Xu Shida,Zhou Jianping,Liu Hao

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference42 articles.

1. Detonative propulsion[J];Wolański;Proc. Combust. Inst.,2013

2. To the question of energy use of detonation combustion[J];Zeldovich;J. Propul. Power,2006

3. Experimental research on the rotating detonation in gaseous fuels–oxygen mixtures[J];Kindracki;Shock Waves,2011

4. N.N. Smirnov, V.F. Nikitin, Y.G. Phylippov, et al. Detonation onset in acetylene–oxygen mixture[J].

5. Characterizing continuously rotating detonation via nonlinear time series analysis[J];He;Proc. Combust. Inst.,2019

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3. Experimental Study of High-Diodicity Inlet Effects on Rotating Detonation Combustor Performance and Operability;Journal of Engineering for Gas Turbines and Power;2024-08-23

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