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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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张新宇 [3]
仲峰泉 [2]
顾洪斌 [2]
Cheng L W [1]
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Indexed By:SCI
Date Issued:2019
Author:张新宇
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Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
Authors:
Zhang X(张旭)
;
Yue LJ(岳连捷)
;
Huang TL(黄庭隆)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
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View/Download:355/125
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Submit date:2020/03/21
Hysteresis
Dual-mode scramjet
Supersonic combustion
Mode transition
Flame stabilization
Combustion oscillation
CH* Luminance Distribution Application and a One-Dimensional Model of the Supersonic Combustor Heat Release Quantization
期刊论文
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2019, 卷号: 36, 期号: 1, 页码: 45-50
Authors:
Wang ZP(王知溥)
;
Gu HB(顾洪斌)
;
Cheng L W
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
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Submit date:2019/04/11
supersonic combustion
one-dimensional modelling
heat release
CH* chemiluminescence
Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 86, 页码: 775-781
Authors:
Zhong FQ(仲峰泉)
;
Cheng LW(程柳维)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
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View/Download:310/94
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Submit date:2019/05/29
Supersonic combustor
Hydrocarbon
Mixture fuel
Flame structure
Ignition