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Large Eddy Simulation of Axisymmetric Scramjet Based on Dynamic Zone Flamelet Model 会议论文
Asia-Pacific International Symposium on Aerospace Technology (APISAT), Korean Soc Aeronaut & Space Sci, Jeju, SOUTH KOREA, NOV 15-17, 2021
作者:  Sun WM(孙文明);  Liu H(刘杭);  Li L(李龙);  Yao W(姚卫)
Adobe PDF(2371Kb)  |  收藏  |  浏览/下载:154/33  |  提交时间:2022/11/24
Axisymmetric scramjet  Ethylene  Improved Delay Detached Eddy Simulation (IDDES)  Dynamic Zone Flamelet Model (DZFM)  Cavity  
A Design Method of Steering Gear Transmission Mechanism Based on Multi-objective Particle Swarm Optimization 会议论文
2021 International Conference on Autonomous Unmanned Systems (ICAUS 2021), Changsha, China, September 24–26, 2021
作者:  Zhuang, Xing;  Wang, Yue;  Li, Dongguang;  Ma YL
Adobe PDF(891Kb)  |  收藏  |  浏览/下载:92/38  |  提交时间:2023/03/17
A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels 会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
作者:  Jin YC(靳一超);  Wu K(吴坤);  Lu Y(陆阳);  Fan XJ(范学军)
Adobe PDF(1121Kb)  |  收藏  |  浏览/下载:149/42  |  提交时间:2022/07/04
Influence of rectangular strips size on aerodynamic performance of a high-speed train subjected to crosswind 会议论文
Fluids Engineering Division Summer Meeting, FEDSM 2021, Virtual, Online, 10 August 2021 到 12 August 2021
作者:  Wang MY(王梦莹);  Sun ZX(孙振旭);  Ju SJ(鞠胜军);  Yang GW(杨国伟)
Adobe PDF(1369Kb)  |  收藏  |  浏览/下载:231/80  |  提交时间:2021/11/30
Aerodynamic performance  Crosswind  High-speed train  Orthogonal design  Rectangular strips  Variance analysis  
Plasma properties measurements of parallel-plane electrodes in Argon by coupling OES and PLIF 会议论文
Global Intelligent Industry Conference, 中国上海, 2020/10/28-30
作者:  Wang FY(王方仪);  Zhang SH(张少华);  Yu XL(余西龙)
Adobe PDF(975Kb)  |  收藏  |  浏览/下载:373/42  |  提交时间:2021/02/01
SOFC-ICE集成热电联产系统的分析、建模与控制 会议论文
2020中国自动化大会, 中国上海, 2020-11-06
作者:  尹海;  程屾;  张健;  高金武
Adobe PDF(577Kb)  |  收藏  |  浏览/下载:190/55  |  提交时间:2021/01/28
热电联产  SOFC-ICE  工作点优化  
Evaluation of the influence of radiation on a GH2/GO2 rocket combustor 会议论文
AIAA Propulsion & Energy Forum, VIRTUAL EVENT, 2020-08-17
作者:  Li B(李波);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1358Kb)  |  收藏  |  浏览/下载:149/45  |  提交时间:2021/02/01
Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model 会议论文
AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020
作者:  Yao W(姚卫);  Chen L(陈留)
Adobe PDF(2272Kb)  |  收藏  |  浏览/下载:259/144  |  提交时间:2021/06/11
A method for rapid generation of 3D infrared radiation intensity field of engine exhaust plume 会议论文
6th Symposium on Novel Optoelectronic Detection Technology and Applications, Beijing, PEOPLES R CHINA, 3 December 2019 through 5 December 2019
作者:  Bao XD(包醒东);  Yu XL(余西龙);  Wang Z.-H;  Mao H.-X;  Xiao Z.-H.
Adobe PDF(602Kb)  |  收藏  |  浏览/下载:150/67  |  提交时间:2021/06/11
Calculation method  Exhaust plume  Infrared spectroscopy  Radiation intensity  Three-dimensional space  
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:212/66  |  提交时间:2021/06/11
concentration  hybrid rocket motor  nozzle exit  temperature  Tunable diode laser absorption spectroscopy (TDLAS)  water vapor