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Numerical study of inflow equivalence ratio inhomogeneity on oblique detonation formation in hydrogen-air mixtures 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 256-263
作者:  Fang YS(方宜申);  Hu ZM(胡宗民);  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Ng HD
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Oblique Detonation  Equivalence Ratio  Mixture Inhomogeneity  Detailed Chemistry  
Uncertain reduced-order modeling for unsteady aerodynamics with interval parameters and its application on robust flutter boundary prediction 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 214-230
作者:  Chen XJ;  Qiu ZP;  Wang XJ;  Li YL;  Wang RX(王睿星)
浏览  |  Adobe PDF(4860Kb)  |  收藏  |  浏览/下载:389/87  |  提交时间:2018/02/08
Uncertain Reduced-order Modeling  Robust Flutter Analysis  Interval Perturbation Method  Uncertain Aeroelastic System  
Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp 期刊论文
PHYSICS OF FLUIDS, 2017, 卷号: 29, 期号: 12, 页码: 125101
作者:  Tong FL(童福林);  Li XL(李新亮);  Duan YH;  Yu ZP(于长平)
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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.
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H2o2/kerosene Bipropellant  Coaxial-swirl Injector  Geometric Constant  Performance  
The stress-velocity relationship of twinning partial dislocations and the phonon-based physical interpretation 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2017, 卷号: 60, 期号: 11
作者:  Wei YJ(魏宇杰);  Peng SY(彭神佑);  Wei, YJ (reprint author), Chinese Acad Sci, Inst Mechan, State Key Lab Nonlinear Mech LNM, Beijing 100190, Peoples R China.;  Wei, YJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Dislocation Mobility  Transverse And Longitudinal Phonons  Subsonic And Supersonic Velocity  Stress-velocity Relationship  Molecular Dynamics  
超声速三维进气道内激波干扰的研究 期刊论文
推进技术, 2017, 期号: 12, 页码: 6
作者:  项高翔;  王春;  汪运鹏;  姜宗林
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高超声速流动  箱式进气道  侧壁压缩进气道  波系结构  流场区域  
高温引气对亚燃冲压燃烧室性能影响的研究 期刊论文
推进技术, 2017, 期号: 12, 页码: 10
作者:  王亚妹;  方祥军;  顾洪斌;  林鹏;  王霄
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亚燃冲压燃烧室  凹腔/支板结构  高温引气  混合效率  燃烧效率  
分辨率优化的混合WENO格式 期刊论文
计算物理, 2017, 卷号: 35, 期号: 4, 页码: 397-404
作者:  郭元;  田奇;  梁贤;  李新亮
浏览  |  Adobe PDF(614Kb)  |  收藏  |  浏览/下载:230/66  |  提交时间:2018/10/24
混合格式  数值耗散  色散  保单调  优化  
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.
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Underexpanded Jets  Noncircular Jets  Nozzle Geometry  Large Eddy Simulation  
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.
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Heat Flux Measurement  Thermocouple  Response Characteristics  Shock Tube