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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 |