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Numerical study on critical axial forces of upheaval buckling for initially stressed submarine pipelines on uneven seabed 期刊论文
OCEAN ENGINEERING, 2017, 卷号: 145, 页码: 344-358
作者:  Xu LG(许雷阁);  Lin M(林缅);  Lin, M (reprint author), Chinese Acad Sci, Inst Mech, Beijing, Peoples R China.
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The Vfife Method  Dimensional Analysis  Upheaval Bucking  Uneven Seabed  
气体体积粘性对二维环形激波聚焦的影响 期刊论文
计算物理, 2017, 卷号: 34, 期号: 04, 页码: 394-402
作者:  李馨东;  赵英奎;  欧阳碧耀;  胡宗民;  姜宗林
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可压缩流动  热完全气体  体积粘性效应  激波聚焦  
Numerical simulation on the marine landslide due to gas hydrate dissociation 期刊论文
ENVIRONMENTAL EARTH SCIENCES, 2017, 卷号: 76, 期号: 4
作者:  Lu XB(鲁晓兵);  Chen XD;  Lu L;  Zhang XH(张旭辉);  Lu, XB (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
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Gas Hydrate  Dissociation Zone  Marine Landslide  
Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
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Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
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Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
可压缩流动中间断问题的高分辨率数值求解方法及应用 学位论文
博士论文,北京: 中国科学院大学, 2017
作者:  刘利
Adobe PDF(16708Kb)  |  收藏  |  浏览/下载:354/12  |  提交时间:2019/05/15
Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
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Combustion  Cost benefit analysis  Costs  Mixtures  Ramjet engines  Supersonic aircraft  Computational costs  Equivalence ratios  Local flow conditions  Scramjet combustors  Statistics approaches  Supersonic combustion  Supersonic combustors  Turbulent combustion  
Assessment of Vibrational Non-Equilibrium Effect on Detonation Cell Size 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2017, 卷号: 189, 期号: 5, 页码: 841-853
作者:  Shi LS;  Shen H;  Zhang P;  Zhang DL(张德良);  Wen CH;  Wen, CY (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China.
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Cellular Structure  Coupled-vibration-chemistry-vibration (Cvcv) Model  Detonation  Two-temperature Model  Vibrational Non-equilibrium  
Development and Fidelity Evaluation of a Skeletal Ethylene Mechanism under Scramjet-Relevant Conditions 期刊论文
ENERGY & FUELS, 2017, 卷号: 31, 期号: 12, 页码: 14296
作者:  Wu K(吴坤);  Yao W(姚卫);  Fan XJ(范学军);  Yao, W;  Fan, XJ
Adobe PDF(1907Kb)  |  收藏  |  浏览/下载:227/76  |  提交时间:2018/07/06
Numerical study on the stratum's responses due to natural gas hydrate dissociation 期刊论文
SHIPS AND OFFSHORE STRUCTURES, 2017, 卷号: 12, 期号: 6, 页码: 775-780
作者:  Lu L;  Zhang XH(张旭辉);  Lu XB(鲁晓兵);  Lu, XB (reprint author), Univ Chinese Acad Sci, Dept Engn Sci, Beijing, Peoples R China.;  Lu, XB (reprint author), Chinese Acad Sci, Inst Mech, Dept LMFS, Beijing, Peoples R China.
Adobe PDF(792Kb)  |  收藏  |  浏览/下载:369/143  |  提交时间:2017/12/27
Gas Hydrate  Dissociation Zone  Slope Instability  Deformation