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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)
Favorite  |  View/Download：10/0  |  Submit date：2024/11/22
Regenerative Cooling  Engine Thrust Chambers  Transcritical Flow and Heat Transfer  Methane Propellant  Review  
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)
Favorite  |  View/Download：5/0  |  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)
Favorite  |  View/Download：62/0  |  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
Favorite  |  View/Download：108/0  |  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)
Favorite  |  View/Download：28/0  |  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)  |  Favorite  |  View/Download：209/10  |  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)  |  Favorite  |  View/Download：118/18  |  Submit date：2024/02/26
Standing oblique detonation  Scramjet engine  Oblique detonation engine  Shock wave  Supersonic combustion  Hypersonic ramjet propulsion  
Numerical Study on the Aerodynamic Heating Characteristics of the Cantilevered Injection System for Oblique Detonation Engine Inlets 期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 10, 页码: 18./通讯作者：Lin, Mingyue
Authors:  Yang F(杨帆);  Lin MY(林明月);  Hu ZM(胡宗民);  Han GL(韩桂来)
Adobe PDF(8946Kb)  |  Favorite  |  View/Download：172/14  |  Submit date：2023/11/28
oblique detonation engine  cantilevered injection  localized high heat flux  boundary layer separation  reattachment  
Combustion Characteristics of a Swirl-Radial-Injection Composite Fuel Grain with Applications in Hybrid Rockets 期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 9, 页码: 19./通讯作者：Lin, Xin, Wang, Zezhong
Authors:  Wang RY(王若岩);  Lin X(林鑫);  Wang ZZ(王泽众);  Wu K(吴坤);  Zhang ZL(张泽林);  Luo JX(罗家枭);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(8125Kb)  |  Favorite  |  View/Download：212/45  |  Submit date：2023/10/30
hybrid rocket engine  swirl-radial injection  regression rate  flame images  combustion efficiency  
Analysis of spray characteristics of a jet film injection element based on Voronoi tessellation 期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 206, 页码: 100-113./通讯作者：Yue, LJ (corresponding author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
Authors:  He CM(何成明);  Zhang, Peng;  He, Zhixia;  Yue LJ(岳连捷)
Adobe PDF(20952Kb)  |  Favorite  |  View/Download：83/8  |  Submit date：2023/04/20
Liquid rocket engine  Pintle injector  Spray characteristics  Jet film injection  Voronoi tessellation