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Theoretical study on the cooling procedure for vertical flow sinters 期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 127, 页码: 592-601
作者:  Pan LS(潘利生);  Wei XL(魏小林);  Peng, Yan;  Ma, Yuejing;  Li B(李博);  Pan, LS (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Vertical Flow Sinter Cooling Device  Sinter Layer  Convection Heat Transfer  Pressure Drop  
The dual information preserving method for stiff reacting flows 期刊论文
COMPUTERS & FLUIDS, 2017, 卷号: 157, 页码: 253-275
作者:  Liu, Li;  Shen YQ(申义庆);  Liu, Shengping;  Yu, Ming;  Shen, YQ (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Stiff Reacting Flow  Dual Information Preserving Method  Numerical Perturbation Method  Shock-capturing Scheme  
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
作者:  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.
Adobe PDF(1708Kb)  |  收藏  |  浏览/下载:447/194  |  提交时间:2017/12/18
H2o2/kerosene Bipropellant  Coaxial-swirl Injector  Geometric Constant  Performance  
Flow characteristic of highly underexpanded jets from various nozzle geometries 期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 125, 页码: 240-253
作者:  Li XP(李晓鹏);  Zhou, Rui;  Yao W(姚卫);  Fan XJ(范学军);  Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(5723Kb)  |  收藏  |  浏览/下载:411/180  |  提交时间:2017/11/16
Underexpanded Jets  Noncircular Jets  Nozzle Geometry  Large Eddy Simulation  
Three-dimensional flame measurements with large field angle 期刊论文
OPTICS EXPRESS, 2017, 卷号: 25, 期号: 18, 页码: 21008-21018
作者:  Wang KL(王宽亮);  Li F(李飞);  Ceng H(曾徽);  Yu XL(余西龙);  Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(2976Kb)  |  收藏  |  浏览/下载:331/112  |  提交时间:2017/11/16
Numerical investigation of the effects of shock tube geometry on the propagation of an ideal blast wave profile 期刊论文
SHOCK WAVES, 2017, 卷号: 27, 期号: 5, 页码: 771-779
作者:  Li, X. D.;  Hu ZM(胡宗民);  Jiang ZL(姜宗林);  Hu, ZM (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Hu, ZM (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Blast Wave Profile  Biological Shock Tube  Blast Overpressure  Geometrical Configuration  
On the response of coaxial surface thermocouples for transient aerodynamic heating measurements 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2017, 卷号: 86, 页码: 141-148
作者:  Li JP(李进平);  Chen H(陈宏);  Zhang SZ(张仕忠);  Zhang XY(张晓源);  Yu HR(俞鸿儒);  Chen, H (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1158Kb)  |  收藏  |  浏览/下载:444/95  |  提交时间:2017/07/24
Heat Flux Measurement  Thermocouple  Response Characteristics  Shock Tube  
Laminar flame speed of lignocellulosic biomass-derived oxygenates and blends of gasoline/oxygenates 期刊论文
FUEL, 2017, 卷号: 202, 页码: 572-582
作者:  Wu Y;  Rossow B;  Modica V;  Yu XL(余西龙);  Wu LL;  Grisch F;  Wu, Y (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
Adobe PDF(1848Kb)  |  收藏  |  浏览/下载:389/138  |  提交时间:2017/08/15
Laminar Flame Speed  Oxygenated Fuels  Gasoline  High Pressure And High Temperature  
Shock relations in gases of heterogeneous thermodynamic properties 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
作者:  Hu ZM(胡宗民);  Zhou K(周凯);  Peng J(彭俊);  Li JP(李进平);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1654Kb)  |  收藏  |  浏览/下载:339/80  |  提交时间:2017/10/25
Shock Wave  Imperfect Gas  Heterogeneous  Theoretical Solution  
Numerical studies of shock wave interactions with a supersonic turbulent boundary layer in compression corner:Turning angle effects 期刊论文
COMPUTERS & FLUIDS, 2017, 卷号: 149, 页码: 56-69
作者:  Tong FL(童福林);  Yu ZP(于长平);  Tang ZG(唐志共);  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.;  Li, XL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
Adobe PDF(6937Kb)  |  收藏  |  浏览/下载:445/158  |  提交时间:2017/10/27
Compression Corner  Low-frequency Oscillation  Coherent Vortex Structure  Power Spectrum  Turbulent Kinetic Energy Budget  Direct Numerical Simulation