科言猫
学术研究的AI总结
首页
文献互助
订阅
我的收藏
科研工具
选题分析
论文总结
专利管理
未登录
返回
林志勇
(Zhiyong Lin)
national university of defense technology - china
25
H指数
51
论文数
1.5K
被引数
0
相关解读
订阅
收录论文
19
发表时间
发表时间
IF
被引数
Diffraction of cellular detonation wave over a cylindrical convex wall
ACTA ASTRONAUTICA
IF
3.4
2020-04-01
11
PRE
AI
Yuan, Xueqiang; Zhou, Jin; Liu, Shijie; Lin, Zhiyong
分享
收藏
Interaction between rotating detonation wave propagation and reactant mixing
ACTA ASTRONAUTICA
IF
3.4
2019-11-01
20
PRE
AI
Sun, Jian; Zhou, Jin; Liu, Shijie; Lin, Zhiyong
分享
收藏
Effects of air injection throat width on a non-premixed rotating detonation engine
ACTA ASTRONAUTICA
IF
3.4
2019-06-01
53
PRE
AI
Sun, Jian; Zhou, Jin; Liu, Shijie; Lin, Zhiyong; Lin, Wei
分享
收藏
Numerical investigation of a non-premixed hollow rotating detonation engine
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
IF
8.3
2019-06-01
47
PRE
AI
Sun, Jian; Zhou, Jin; Liu, Shijie; Lin, Zhiyong; Lin, Wei
分享
收藏
Numerical investigation of a rotating detonation engine under premixed/non-premixed conditions
预混/非预混条件下旋转爆震发动机的数值研究
ACTA ASTRONAUTICA
IF
3.4
2018-11-01
68
PRE
AI
Sun, Jian; Zhou, Jin; Liu, Shijie; Lin, Zhiyong
分享
收藏
Plume flowfield and propulsive performance analysis of a rotating detonation engine
AEROSPACE SCIENCE AND TECHNOLOGY
IF
5.8
2018-10-01
43
PRE
AI
Sun, Jian; Zhou, Jin; Liu, Shijie; Lin, Zhiyong; Lin, Wei
分享
收藏
The initiation and propagation of detonation in supersonic combustible flow with boundary layer
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
IF
8.3
2018-07-01
11
PRE
AI
Chen, Weiqiang; Liang, Jianhan; Cai, Xiaodong; Lin, Zhiyong
分享
收藏
Effects of dynamic backpressure on shock train motions in straight isolator
ACTA ASTRONAUTICA
IF
3.4
2017-12-01
31
PRE
AI
Cai, Jianhua; Zhou, Jin; Liu, Shijie; Lin, Zhiyong
分享
收藏
Effects of injection nozzle exit width on rotating detonation engine
ACTA ASTRONAUTICA
IF
3.4
2017-11-01
66
PRE
AI
Sun, Jian; Zhou, Jin; Liu, Shijie; Lin, Zhiyong; Cai, Jianhua
分享
收藏
Detonation simulations in expanding channel with supersonic combustible mixture
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
IF
8.3
2017-03-01
12
PRE
AI
Chen, Weiqiang; Liang, Jianhan; Cai, Xiaodong; Lin, Zhiyong
分享
收藏
Numerical study of detonation diffraction through 90-degree curved channels to expansion area
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
IF
8.3
2017-03-01
16
PRE
AI
Yuan, Xueqiang; Zhou, Jin; Lin, Zhiyong; Cai, Xiaodong
分享
收藏
Adaptive simulations of detonation propagation in 90-degree bent tubes
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
IF
8.3
2016-10-01
22
PRE
AI
Yuan, Xueqiang; Zhou, Jin; Lin, Zhiyong; Cai, Xiaodong
分享
收藏
Adaptive simulations of cavity-based detonation in supersonic hydrogen-oxygen mixture
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
IF
8.3
2016-05-01
20
OA
AI
Cai, Xiaodong; Liang, Jianhan; Deiterding, Ralf; Lin, Zhiyong
分享
收藏
Adaptive mesh refinement based simulations of three-dimensional detonation combustion in supersonic combustible mixtures with a detailed reaction model
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
IF
8.3
2016-01-01
50
OA
AI
Cai, Xiaodong; Liang, Jianhan; Deiterding, Ralf; Che, Yonggang; Lin, Zhiyong
分享
收藏
Experimental verification of air-breathing continuous rotating detonation fueled by hydrogen
以氢为燃料的空气呼吸连续旋转爆轰的实验验证
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
IF
8.3
2015-08-01
67
PRE
AI
Wang, Chao; Liu, Weidong; Liu, Shijie; Jiang, Luxin; Lin, Zhiyong
分享
收藏
Experimental study on propagation mode of H2/Air continuously rotating detonation wave
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
IF
8.3
2015-01-01
123
PRE
AI
Lin, Wei; Zhou, Jin; Liu, Shijie; Lin, Zhiyong; Zhuang, Fengchen
分享
收藏
Effects of a hot jet on detonation initiation and propagation in supersonic combustible mixtures
ACTA ASTRONAUTICA
IF
3.4
2014-12-01
23
PRE
AI
Liang, Jianhan; Cai, Xiaodong; Lin, Zhiyong; Deiterding, Ralf
分享
收藏
Parametric study of detonation initiation using a hot jet in supersonic combustible mixtures
在超音速可燃混合物中使用热射流对爆炸起爆的参数研究
AEROSPACE SCIENCE AND TECHNOLOGY
IF
5.8
2014-12-01
31
PRE
AI
Cai, Xiaodong; Liang, Jianhan; Lin, Zhiyong; Deiterding, Ralf; Liu, Yu
分享
收藏
Deflagration-to-Detonation Transition Induced by Hot Jets in a Supersonic Premixed Airstream
CHINESE PHYSICS LETTERS
IF
4.2
2013-05-10
19
PRE
AI
Han Xu; Zhou Jin; Lin Zhi-Yong; Liu Yu
分享
收藏
研究方向
连续爆震发动机基础与应用研究,燃烧流场激光诊断技术应用
航空宇航科学与技术
工作经历 2019.08 中山大学航空航天大学 教授
学术团体任职
Engines and Propulsion
教学经历
2019- 《航空航天工程导论》 本科生必修程
2020~ 《火箭推进原理》 本科生专业必修程
2023- 《高超声速推进技术》 研究生课程
科研项目(部分)
燃料斜爆震发动机方案设计
高超声速测试
Ø 2021.1-2022.3,宽域冲压技术研究,项目负责人
爆震燃烧
空天发动机
吸气式连续旋转爆震发动机技术
发明专利(部分)
一种用于超声速研究的高速预混火焰炉 2013.5授权
代表性部分论文
合作学者
合作期刊
王
王超
(Chao Wang)
H 指数: 49 · 论文数: 1.3K
R
Ralf Deiterding
H 指数: 31 · 论文数: 215
S
Shijie Liu
H 指数: 30 · 论文数: 106
J
Jianhan Liang
H 指数: 26 · 论文数: 134
J
Jin Zhou
H 指数: 24 · 论文数: 122
查看更多