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低温燃烧和能源未来发展需求 科普文章
2017
Authors:  何郁编写
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超高速流动模拟及热化学反应模型对比研究 期刊论文
北京航空航天大学学报, 2017, 卷号: 43, 期号: 06, 页码: 1173-1181
Authors:  周凯;  李旭东;  胡宗民;  姜宗林
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超高速  膨胀管  数值模拟  热化学反应模型  适用范围  
Theories and technologies for duplicating hypersonic flight conditions for ground testing 期刊论文
NATIONAL SCIENCE REVIEW, 2017, 卷号: 4, 期号: 3, 页码: 290-U461
Authors:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing, Peoples R China.;  Jiang, ZL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing, Peoples R China.
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A low-dissipation solver based on OpenFOAM designed for large eddy simulation in compressible flows 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
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Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems  
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Fan XJ(范学军);  Fan, Xuejun(xfan@imech.ac.cn)
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Adiabatic Flame Temperature  Aerodynamics  Boundary Layer Flow  Boundary Layers  Chemical Analysis  Combustion  Computational Chemistry  Directed Graphs  Flow Separation  Mach Number  Principal Component Analysis  Regression Analysis  Sensitivity Analysis  Spacecraft  Supersonic Aerodynamics  Supersonic Aircraft  Transients  
A low-dissipation scheme based on OpenFoam designed for large eddy simulation in compressible flow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军);  Yao, Wei(weiyao@imech.ac.cn)
View  |  Adobe PDF(1358Kb)  |  Favorite  |  View/Download：455/116  |  Submit date：2018/01/16
Computational Fluid Dynamics  Computer Software  Digital Storage  Kinetic Energy  Kinetics  Open Source Software  Open Systems  Runge Kutta Methods  Shock Tubes  Shock Waves  Spacecraft  Turbulence  Two Phase Flow  
Full Scale Detached Eddy Simulation of Transverse Hydrogen Jet in Supersonic Combustion 会议论文
53rd AIAA/SAE/ASEE Joint Propulsion Conference , Atlanta, GA., 10-12 July 2017
Authors:  Fan E;  Wu K(吴坤);  Lee YC;  Yao W(姚卫);  Fan XJ(范学军)
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高压捕获翼新型气动构型研究 学位论文
博士论文，北京: 中国科学院大学, 2017
Authors:  李广利
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超临界压力下航空煤油流动与传热特性研究 学位论文
博士论文，北京: 中国科学院大学, 2017
Authors:  张永江
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三维激波干扰理论与应用研究 学位论文
博士论文，北京: 中国科学院大学, 2017
Authors:  项高翔
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