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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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Simple shape model for normal shock trains in straight channels
期刊论文
THEORETICAL AND COMPUTATIONAL FLUID DYNAMICS, 2025, 卷号: 39, 期号: 1, 页码: 16./通讯作者:Chen, Hao, Yue, Lianjie
Authors:
Yu FY(于方游)
;
Huang, Tinglong
;
Chen H(陈昊)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
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View/Download:389/0
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Submit date:2025/02/17
Shock train
Mathematical model
Shock reflection
Isolator
Ramjet engine
Computational investigation on the formation of liquid-fueled oblique detonation waves
期刊论文
COMBUSTION AND FLAME, 2025, 卷号: 271, 页码: 113839./通讯作者:Hu ZM, Zhang P
Authors:
Wang WH(王文浩)
;
Hu ZM(胡宗民)
;
Zhang, Peng
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View/Download:49/0
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Submit date:2024/12/02
Oblique detonation wave engine
Liquid-fueled detonation
Droplet breakup
Vapor blending
On-wedge strip
OpenFOAM
Fundamental research progress in regenerative cooling for methane engine thrust chambers
期刊论文
APPLIED THERMAL ENGINEERING, 2025, 卷号: 258, 页码: 16./通讯作者:Wei, Xiaolin
Authors:
Yao Y(姚远)
;
Chen, Qi
;
Bin F(宾峰)
;
Qiu, Yinan
;
Yang, Zhiqiang
;
Zhao, Yanxing
;
Wei XL(魏小林)
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View/Download:68/0
  |  
Submit date:2024/11/22
Regenerative Cooling
Engine Thrust Chambers
Transcritical Flow and Heat Transfer
Methane Propellant
Review
A multi-layer Kriging surrogate model for the reliability analysis of variable stator vanes in aero engines
期刊论文
AERONAUTICAL JOURNAL, 2024, 页码: 21./通讯作者:Fan, J.
Authors:
Fan, J
;
Xu, H
;
Meng, Q
;
Xu SH(徐升华)
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View/Download:557/0
  |  
Submit date:2025/02/10
surrogate model
reliability analysis
vane stator variables
aero-engine
Exploration of initiation and stabilization properties of oblique detonation in a combustor with hydrogen fuel pre-injection
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2024, 卷号: 91, 页码: 584-595./通讯作者:Xiang, Gaoxiang
Authors:
Xin, Yirong
;
Jiang, Ziqi
;
Guo, Shuaishuai
;
Shen, Lihui
;
Xiang, Gaoxiang
;
Wang Q(汪球)
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  |  
View/Download:57/0
  |  
Submit date:2024/11/22
Fuel pre-injection
Oblique detonation engine
Standing detonation
Combustor
Enhanced fast inertial relaxation engine (FIRE) for multiscale simulations
期刊论文
COMPUTATIONAL MATERIALS SCIENCE, 2024, 卷号: 244, 页码: 12./通讯作者:Xiao, Pan
Authors:
Tang MJ(唐明健)
;
Shuang, Fei
;
Xiao P(肖攀)
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View/Download:89/0
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Submit date:2024/08/23
Multiscale structural relaxation
Fast inertial relaxation engine
Atomistic to continuum coupling
Study on the propulsive performance of oblique detonation engine
期刊论文
ENERGY, 2024, 卷号: 292, 页码: 11./通讯作者:Liu, Yunfeng
Authors:
Liu YF(刘云峰)
;
Han, Xin
;
Zhang, Zijian
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View/Download:157/0
  |  
Submit date:2024/04/15
Oblique detonation engine
ODE
Propulsive performance
Specific impulse
Regression Rate and Combustion Efficiency of Composite Hybrid Rocket Grains Based on Modular Fuel Units
期刊论文
AEROSPACE, 2024, 卷号: 11, 期号: 4, 页码: 18./通讯作者:Lin, Xin, Wang, Zezhong
Authors:
Pan JJ(潘俊杰)
;
Lin X(林鑫)
;
Wang ZZ(王泽众)
;
Wang RY(王若岩)
;
Wu K(吴坤)
;
Liang, Jinhu
;
Yu XL(余西龙)
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View/Download:37/0
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Submit date:2024/05/27
modular unit
modification
regression rate
combustion efficiency
hybrid rocket engine
Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades
期刊论文
VIRTUAL AND PHYSICAL PROTOTYPING, 2023, 卷号: 18, 期号: 1, 页码: e2235680./通讯作者:Lin, X (corresponding author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Authors:
Qu DD(屈丹丹)
;
Lin X(林鑫)
;
Zhang K(张坤)
;
Li ZY(李志永)
;
Wang ZZ(王泽众)
;
Liu GL(刘国亮)
;
Meng Y(孟洋)
;
Luo GX(罗耕星)
;
Wang RY(王若岩)
;
Yu XL(余西龙)
Adobe PDF(4980Kb)
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View/Download:273/56
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Submit date:2023/09/05
Hybrid rocket engine
additive manufacturing
three-dimensional printing
breathable blade
composite fuel grain
mechanical and combustion properties
porous structure
>
Standing oblique detonation for hypersonic propulsion: A review
期刊论文
PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17./通讯作者:Jiang, Zonglin
Authors:
Jiang ZL(姜宗林)
Adobe PDF(10386Kb)
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View/Download:153/31
  |  
Submit date:2024/02/26
Standing oblique detonation
Scramjet engine
Oblique detonation engine
Shock wave
Supersonic combustion
Hypersonic ramjet propulsion