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Temperature and H2O concentration measurements for a hybrid rocket motor plume using a single mid-infrared tunable diode laser 会议论文
2020 Applied Optics and Photonics China: Optical Sensing and Imaging Technology, AOPC 2020, Xiamen, PEOPLES R CHINA, 25 August 2020 through 27 August 2020
作者:  Fang SH(方思晗);  Wang ZZ(王泽众);  Li RJ(李仁杰);  Zhang ZL(张泽林);  Lin X(林鑫);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(1569Kb)  |  收藏  |  浏览/下载：216/67  |  提交时间：2021/06/11
concentration  hybrid rocket motor  nozzle exit  temperature  Tunable diode laser absorption spectroscopy (TDLAS)  water vapor  
Rebuilding experimental nonequilibrium radiation in shock-heated Martian-like mixture flows using electronic state-to-state approach 会议论文
8th International Symposium on Physics of Fluids (ISPF), Xian, PEOPLES R CHINA, JUN 10-13, 2019
作者:  Hong QZ(洪启臻);  Wang XY(王小永);  Hu Y(胡远);  Lin X(林鑫);  Sun QH(孙泉华)
Adobe PDF(749Kb)  |  收藏  |  浏览/下载：78/39  |  提交时间：2022/11/24
Electronic state-to-state approach  nonequilibrium radiation  Martian-like mixture  
Spectral Radiant Intensity Calculation of Air in Shock Tube 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Lyu, Jun Ming;  Cheng, X. L.;  Yu, J. J.;  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(791Kb)  |  收藏  |  浏览/下载：64/23  |  提交时间：2023/03/17
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
作者:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Wu K(吴坤);  Fan XJ(范学军)
浏览  |  Adobe PDF(805Kb)  |  收藏  |  浏览/下载：395/147  |  提交时间：2018/06/06
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
作者:  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1377Kb)  |  收藏  |  浏览/下载：280/113  |  提交时间：2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems  
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
作者:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军);  Yao, Wei(weiyao@imech.ac.cn)
Adobe PDF(1358Kb)  |  收藏  |  浏览/下载：424/107  |  提交时间：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  
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)
Adobe PDF(1249Kb)  |  收藏  |  浏览/下载：300/89  |  提交时间：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
A low-dissipation solver based on openFOAM designed for large eddy simulation in compressible flow 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:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1377Kb)  |  收藏  |  浏览/下载：483/93  |  提交时间：2018/11/08
Computational Fluid Dynamics  Digital Storage  Kinetic Energy  Kinetics  Open Source Software  Open Systems  Ramjet Engines  Runge Kutta Methods  Shock Tubes  Turbulence  Two Phase Flow  Bench  Mark Problems  Central  Upwind Scheme  Computational Fluid Dynamics Software  Skew  Symmetric Forms  Temporal Discretization  Turbulence Structures  Unstructured Meshes  Wall Bounded Turbulence  
Theoretical calculation of mid-infrared spectra from hypersonic non-ablative sphere 会议论文
International Symposium on Infrared Technology and Application / International Symposium on Robot Sensing and Advanced Control, Beijing, PEOPLES R CHINA, MAY 09-11, 2016
作者:  Wu J;  Yu XL(余西龙);  Zhu XJ;  Ma J;  Mao HX;  Wu, J (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Wu, J (reprint author), Sci & Technol Opt Radiat Lab, Beijing 100854, Peoples R China.
Adobe PDF(1160Kb)  |  收藏  |  浏览/下载：279/85  |  提交时间：2017/05/12
Hypersonic  Mid-infrared  Atom  Diatomic Molecule  Partition-functions  Molecules  Air  
Experimental and Modeling Investigation of CO2 Dissociation in Mars Entry Condition 会议论文
18th International Conference on the Methods of Aerophysical Research (ICMAR), Perm Natl Res Polytechn Univ, Perm, RUSSIA, JUN 27-JUL 03, 2016
作者:  Lin X;  Chen LZ;  Peng JL;  Li JP(李进平);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(1399Kb)  |  收藏  |  浏览/下载：292/82  |  提交时间：2017/05/12
Nonequilibrium