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C

Chibing Shen

national university of defense technology - china

21H指数
78论文数
1.2K被引数
收录论文 33
发表时间
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Experimental exploration on the performance of the secondary recirculation jet for the shock wave/boundary layer interaction and mixing augment in supersonic crossflow对激波/边界层相互作用及超音速交叉流中混合增强的二次回流射流性能的实验探索
errAerospace Science and Technology
IF5.8
err2026-03-09
err0
PREAI
errZhao-bo Du; Chi-bing Shen; Wei Huang; Xiao-ping Xu; Feng Wei; Xiao-ting Yan; Wen-yuan Yang
err分享
err收藏
Effect of Injector Recess Depth on Flame Structure of Single Injector in Air Heater单喷嘴空气加热器中喷嘴内凹深度对火焰结构的影响
errAerospace
IF2.2
err2025-12-25
err0
PREAI
errWang, Ke; Shen, Chibing; Fan, Bo
err分享
err收藏
Numerical and experimental exploration on the strut-cavity flow characteristics induced by the oblique shock wave in supersonic crossflow超声速交叉流中斜激波诱导的撑杆-空腔流特性的数值与实验探索
errAerospace Science and Technology
IF5.8
err2025-11-24
err0
PREAI
errZhao-bo Du; Chi-bing Shen; Wei Huang; Xiao-ping Xu; Shan-shan Tian; Liang Ma; Yan Zhao
err分享
err收藏
Ignition dynamics in a hollow supersonic combustor with parallel-cavity using LES带有平行腔的空心超燃燃烧室中的点火动力学研究（采用大涡模拟方法）
errActa Astronautica
IF3.4
err2025-11-07
err0
PREAI
errZhiqun Meng; Chibing Shen; Kaijing Jia; Jiaoru Wang; Haoming He
err分享
err收藏
Numerical study on flame stabilization by shock-induced in a supersonic combustor with parallel-cavity: Symmetric configuration超声速燃烧室中平行腔对称构型下激波诱导火焰稳定性的数值研究
errACTA ASTRONAUTICA
IF3.4
err2025-07-01
err0
PREAI
errMeng, Zhiqun; Shen, Chibing; Jia, Kaijing; He, Haoming
err分享
err收藏
Influence of momentum ratio control mode on spray and combustion characteristics of a LOX/LCH4 pintle injector ( vol 23, pg 415, 2022)
errzhejiang university science b
IF3.9
err2024-12-11
err0
PREAI
errZhou, Rui; Shen, Chi-bing
err分享
err收藏
Numerical study on the mixing enhancement induced by the interaction between the hydrogen/ air coaxial jets and oblique shock wave at Mach 3 supersonic crossflow
errINTERNATIONAL JOURNAL OF HYDROGEN ENERGY
IF8.3
err2023-11-01
err2
PREAI
errTang, Hao-ran; Shen, Chi-bing; Du, Zhao-bo; Huangfu, Hui-dong; Xiong, Si-jin; Zhang, Peng
err分享
err收藏
Experimental study on the combustion characteristics of LOX/LCH4 pintle injectors
errFUEL
IF7.5
err2023-05-01
err13
PREAI
errShen, Chibing; Zhou, Rui
err分享
err收藏
Control mechanism of the three-dimensional shock wave/boundary layer interaction with the steady and pulsed micro-jets in a supersonic crossflow
errPHYSICS OF FLUIDS
IF4.3
err2022-08-17
err24
PREAI
errDu, Zhao-bo; Shen, Chi-bing; Huang, Wei; Fan, Bo; Han, Yi
err分享
err收藏
Influence of momentum ratio control mode on spray and combustion characteristics of a LOX/LCH4 pintle injector
errzhejiang university science b
IF3.9
err2022-05-27
err5
PREAI
errZhou, Rui; Shen, Chi-bing
err分享
err收藏
Experimental study on the spray characteristics of a pintle injector element
errACTA ASTRONAUTICA
IF3.4
err2022-05-01
err22
errOAAI
errZhou, Rui; Shen, Chibing
err分享
err收藏
Hydrogen mixing augmentation mechanism induced by the vortex generator and oblique shock wave in a scramjet engine
errINTERNATIONAL JOURNAL OF HYDROGEN ENERGY
IF8.3
err2022-05-01
err8
PREAI
errDu, Zhao-bo; Shen, Chi-bing; Huang, Wei; Wu, Han; Tang, Hao-Ran; Yang, Jia-ning
err分享
err收藏
Investigation on the impact of the induced shock wave on the hydrogen mixing augmentation in a supersonic crossflow: A numerical study
errFUEL
IF7.5
err2022-03-01
err24
PREAI
errDu, Zhao-bo; Shen, Chi-bing; Huang, Wei; Han, Yi
err分享
err收藏
Mixing augmentation induced by the combination of the oblique shock wave and secondary recirculation jet in a supersonic crossflow
errINTERNATIONAL JOURNAL OF HYDROGEN ENERGY
IF8.3
err2022-02-01
err14
PREAI
errDu, Zhao-bo; Shen, Chi-bing; Huang, Wei; Zhong, Xiang-yu
err分享
err收藏
Design exploration on the shock wave/turbulence boundary layer control induced by the secondary recirculation jet二次再循环射流引起的休克波/湍流边界层控制的设计探索
errACTA ASTRONAUTICA
IF3.4
err2021-04-01
err31
PREAI
errDu, Zhao-bo; Shen, Chi-bing; Shen, Yang; Huang, Wei; Yan, Li
err分享
err收藏
Parametric study on mixing augmentation mechanism induced by cantilevered ramp injectors in a shock-induced combustion ramjet engine
errAEROSPACE SCIENCE AND TECHNOLOGY
IF5.8
err2021-01-01
err43
PREAI
errDu, Zhao-bo; Shen, Chi-bing; Huang, Wei; Yan, Li; Liang, Jian-han; Choubey, Gautam
err分享
err收藏
Numerical study on the morphology of a liquid-liquid pintle injector element primary breakup spray
errzhejiang university science b
IF3.9
err2020-09-30
err16
PREAI
errZhou, Rui; Shen, Chi-bing; Jin, Xuan
err分享
err收藏
Turbulent structures and mixing enhancement with lobed mixers in a supersonic mixing layer
errPHYSICS OF FLUIDS
IF4.3
err2020-04-10
err20
PREAI
errFang, Xin-xin; Shen, Chi-bing; Sun, Ming-bo; Wang, Hong-bo; Wang, Peng
err分享
err收藏
Characteristics of mixing enhancement achieved using a pulsed plasma synthetic jet in a supersonic flow
errzhejiang university science b
IF3.9
err2019-09-06
err26
PREAI
errWang, Peng; Shen, Chi-bing
err分享
err收藏
Study on ignition process of air/liquid oxygen/ethanol tripropellant coaxial jets in a subscale air heater
errACTA ASTRONAUTICA
IF3.4
err2019-09-01
err2
PREAI
errShen, Chibing; Yuan, Lei
err分享
err收藏

研究方向

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合作学者
合作期刊
W
Wei Huang
H 指数: 61 · 论文数: 357
M
Mingbo Sun
H 指数: 53 · 论文数: 397
刘
刘军 (Jun Liu)
H 指数: 50 · 论文数: 942
L
Li Yan
H 指数: 45 · 论文数: 103
R
Richard D. Sandberg
H 指数: 42 · 论文数: 472
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