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面向高超声速飞行的激波诱燃宏观流动及微观机理分析 学位论文
博士论文,北京: 中国科学院大学, 2022
Authors:  马凯夫
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激波诱导燃烧  氢氧燃烧  热化学非平衡  微观机理  激波诱燃发动机  
Multispectral infrared absorption spectroscopy for quantitative temperature measurements in axisymmetric laminar premixed sooting flames 期刊论文
CASE STUDIES IN THERMAL ENGINEERING, 2021, 卷号: 28, 页码: 11
Authors:  Ma, Liuhao;  Duan, Kun;  Cheong, Kin-Pang;  Yuan CK(苑朝凯);  Ren, Wei
Adobe PDF(5899Kb)  |  Favorite  |  View/Download:280/70  |  Submit date:2021/11/29
Temperature measurement  Sooting flame  Multispectral infrared absorption spectroscopy  Optical sensing  
超燃冲压发动机加速过程及等离子体对超声速火焰结构的影响 学位论文
博士论文,北京: 中国科学院大学, 2019
Authors:  孟宇
Adobe PDF(11443Kb)  |  Favorite  |  View/Download:734/44  |  Submit date:2019/11/07
超燃冲压发动机,燃烧模态,火焰结构,加速过程,微波,滑移电弧,等离子体  
Hypergolic ignition modulated by head-on collision, intermixing and convective cooling of binary droplets with varying sizes 期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2019, 卷号: 139, 页码: 475-481
Authors:  Zhang DW;  Yu DH;  Zhang P;  Yuan YM(袁越明);  Yue LJ(岳连捷);  Zhang TC(张泰昌);  Fan XJ(范学军)
View  |  Adobe PDF(1528Kb)  |  Favorite  |  View/Download:354/131  |  Submit date:2019/09/09
Numerical study of chemically reacting flow in a shock tube using a high-order point-implicit scheme 期刊论文
COMPUTERS & FLUIDS, 2019, 卷号: 184, 页码: 107-118
Authors:  Chen S;  Sun QH(孙泉华);  Klioutchnikov I;  Olivier H
View  |  Adobe PDF(1365Kb)  |  Favorite  |  View/Download:350/133  |  Submit date:2019/06/10
Shock wave/boundary-layer interactions  Real gas effects  Chemical nonequilibrium  High-order scheme  
基于简化机理的超声速点火与火焰特性非定常数值研究 学位论文
博士论文,北京: 中国科学院大学, 2018
Authors:  马素刚
Adobe PDF(17418Kb)  |  Favorite  |  View/Download:607/19  |  Submit date:2018/05/28
碳氢燃料  超声速燃烧  大涡模拟  火焰面模型  简化反应机理  
Measurement of multispecies concentration and gas temperature in an ammonium-dinitramide-based thruster by tunable diode lasers 期刊论文
APPLIED OPTICS, 2018, 卷号: 57, 期号: 6, 页码: 1321-1330
Authors:  Zeng H(曾徽);  Li F(李飞);  Yu XL(余西龙);  Ou DB;  Chen LZ
View  |  Adobe PDF(2664Kb)  |  Favorite  |  View/Download:497/111  |  Submit date:2018/10/30
The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 70, 页码: 636-643
Authors:  Li HX(李慧鑫);  Ye L(叶亮);  Wei XL(魏小林);  Li T(李腾);  Li S(李森);  Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1708Kb)  |  Favorite  |  View/Download:503/218  |  Submit date:2017/12/18
H2o2/kerosene Bipropellant  Coaxial-swirl Injector  Geometric Constant  Performance  
Experimental Studies of Film Cooling in Supersonic Combustors 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Fan C(樊川);  Wang J(王晶);  Fan XJ(范学军)
View  |  Adobe PDF(735Kb)  |  Favorite  |  View/Download:351/120  |  Submit date:2018/01/16
Combustion  Combustors  Coolants  Kerosene  Spacecraft  Supersonic Aerodynamics  
Multispecies Absorption Measurement in an Ammonium Dinitramide based Thruster 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Zeng W(曾徽);  Lin X(林鑫);  Zhen RP;  Chen LZ;  Li F(李飞);  Yu XL(余西龙);  Li, Fei(lifei@imech.ac.cn)
View  |  Adobe PDF(897Kb)  |  Favorite  |  View/Download:509/112  |  Submit date:2018/01/16
Combustion  Gas Absorption  Infrared Devices  Monopropellants  Optical Parametric Oscillators  Spacecraft