IMECH-IR

浏览/检索结果: 共19条,第1-10条 帮助

限定条件                    
已选(0)清除 条数/页:   排序方式:
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:151/42  |  提交时间:2022/07/04
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:215/67  |  提交时间:2021/06/11
concentration  hybrid rocket motor  nozzle exit  temperature  Tunable diode laser absorption spectroscopy (TDLAS)  water vapor  
Validation and application of gas radiation computation at earth re-entry conditions 会议论文
31st International Symposium on Rarefied Gas Dynamics, RGD 2018, University of StrathclydeGlasgow; United Kingdom;, 23 July 2018 ~ 27 July 2018
作者:  Lyu JM;  Cheng XL;  Yu JJ;  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(2168Kb)  |  收藏  |  浏览/下载:249/70  |  提交时间:2020/11/20
Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
作者:  Yao W(姚卫);  Li B(李波)
Adobe PDF(1665Kb)  |  收藏  |  浏览/下载:140/43  |  提交时间:2020/11/20
Dynamic zone flamelet model  GH2/GO2  Large Eddy Simulation (LES)  Rocket combustor  Turbulence-chemistry interaction  
Supercritical GN2/GH2 jet modeled by the ECS method 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
作者:  Yao W(姚卫);  Jin YC(靳一超);  Lee YC(李亚超)
Adobe PDF(1048Kb)  |  收藏  |  浏览/下载:153/57  |  提交时间:2020/11/20
Ventilated partial cavitating flow around a blunt body near the free surface 会议论文
16th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2016, Honolulu, HI, United states, April 10, 2016 - April 15, 2016
作者:  Wang YW(王一伟);  Wu XC(吴小翠);  Huang CG(黄晨光)
浏览  |  Adobe PDF(757Kb)  |  收藏  |  浏览/下载:182/40  |  提交时间:2019/11/20
Axisymmetric bodies  Cavity boundaries  Free surfaces  High  speed underwater vehicles  Launching systems  Media properties  Unsteady behaviors  Ventilated cavitation  
Optimization of the self-condensing CO2 transcritical power cycle using solar thermal energy 会议论文
10th International Conference on Applied Energy (ICAE), Hong Kong, HONG KONG, AUG 22-25, 2018
作者:  Pan LS(潘利生);  Li,Bing;  Shi,Weixiu;  Wei XL(魏小林)
Adobe PDF(1140Kb)  |  收藏  |  浏览/下载:96/31  |  提交时间:2022/11/24
CO2 transcritical power cycle  Supercritical CO2 Brayton cycle  Solar thermal energy  CO2 condensation  
Influence of Chemical Mechanisms on Supersonic Combustion Characteristics Fueled by Kerosene 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio, July 9-11, 2018
作者:  Yao W(姚卫);  Wu K(吴坤);  Lee YC(李亚超);  Fan XJ(范学军)
Adobe PDF(1156Kb)  |  收藏  |  浏览/下载:414/0  |  提交时间:2018/12/26
Real-gas Effect Accounted for by the Principle of Extended Corresponding States in Modeling Supersonic Kerosene Jet 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
作者:  Wang Y;  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1120Kb)  |  收藏  |  浏览/下载:486/103  |  提交时间:2018/12/26
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