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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  
Experimental Research on the Detonation in Gaseous Mixtures with Suspended Aluminum Particles 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Zhang XY(张晓源);  Chen H(陈宏);  Li JP(李进平);  Zhang SZ(张仕忠);  Yu HR(俞鸿儒)
Adobe PDF(543Kb)  |  收藏  |  浏览/下载：36/18  |  提交时间：2023/03/17
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  
Prediction of kerosene properties at supercritical pressures by Artificial Neural Network 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
作者:  Li B;  Lee YC(李亚超);  Yao W(姚卫);  Lu Y(陆阳);  Fan XJ(范学军)
浏览  |  Adobe PDF(1813Kb)  |  收藏  |  浏览/下载：305/82  |  提交时间：2018/12/26
Prediction of kerosene properties at supercritical pressures by Artificial Neural Network 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio., July 9-11, 2018
作者:  Li B(李波);  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1813Kb)  |  收藏  |  浏览/下载：173/64  |  提交时间：2020/08/27
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：393/147  |  提交时间：2018/06/06
Multispecies Absorption Measurement in an Ammonium Dinitramide based Thruster 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Zeng W(曾徽);  Lin X(林鑫);  Zhen RP;  Chen LZ;  Li F(李飞);  Yu XL(余西龙);  Li, Fei(lifei@imech.ac.cn)
浏览  |  Adobe PDF(897Kb)  |  收藏  |  浏览/下载：452/97  |  提交时间：2018/01/16
Combustion  Gas Absorption  Infrared Devices  Monopropellants  Optical Parametric Oscillators  Spacecraft  
Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015
作者:  Lu Y(陆阳);  Wang XZ(王新竹);  Li L(李龙);  Cheng D(程迪);  Yuan T(袁涛);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(445Kb)  |  收藏  |  浏览/下载：427/92  |  提交时间：2016/01/08
Hydrocarbons  Combustors  Cooling  Heat Transfer