中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共10条，第1-10条 帮助

限定条件            
已选(0)清除 条数/页：   排序方式：
Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Cheng LW(程柳维);  Zhong FQ(仲峰泉);  Wang ZP(王知溥);  Gu HB(顾洪斌);  Ma SG(马素刚);  Zhang XY(张新宇)
浏览  |  Adobe PDF(517Kb)  |  收藏  |  浏览/下载：310/100  |  提交时间：2018/01/16
Combustors  Cracks  Diesel Engines  Efficiency  Ethylene  Fighter Aircraft  Fuels  High Speed Cameras  Ignition  Kerosene  Luminance  Spacecraft  Stabilization  
基于CN 的火星再入流场转动温度和振动温度测量 会议论文
LHD2013夏季学术研讨会, 河北平山, 2013
作者:  林鑫;  余西龙;  李飞;  张少华;  张新宇
Adobe PDF(625Kb)  |  收藏  |  浏览/下载：648/203  |  提交时间：2014/01/23
发射光谱  火星再入  转动温度  振动温度  
Combined TDLAS and OES technique for CO concentration measurement in shock-heated Martian atmosphere 会议论文
2nd International Symposium on Laser Interaction with Matter (LIMIS), Xian, PEOPLES R CHINA, SEP 09-12, 2012
作者:  Lin X(林鑫);  Yu XL(余西龙);  Li F(李飞);  Zhang SH(张少华);  Xin JG;  Zhang XY(张新宇);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(683Kb)  |  收藏  |  浏览/下载：790/276  |  提交时间：2013/12/12
Optical Emission Spectroscopy (Oes)  Tunable Diode Laser Absorption Spectroscopy (Tdlas)  Shock Wave  Temperature  Concentration  
自由射流台喷管出口参数的吸收光谱诊断 会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
作者:  李飞;  余西龙;  李东霞;  陈立红;  张新宇
Adobe PDF(1474Kb)  |  收藏  |  浏览/下载：521/150  |  提交时间：2014/01/23
自由射流台  可调谐二极管吸收光谱技术(Tdlas)  温度测量  
Measurement of temperature, velocity and water vapor concentration in a scramjet combustor based on nearinfrared diode laser absorption 会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
作者:  Li F(李飞);  Yu XL(余西龙);  Gu HB(顾洪斌);  Li Z(李智);  Chen LH(陈立红);  Zhang XY(张新宇);  Li F(李飞)
浏览  |  Adobe PDF(420Kb)  |  收藏  |  浏览/下载：593/197  |  提交时间：2014/02/24
激光诱导CH荧光在燃烧诊断中初步应用 会议论文
第三届高超声速科技学术会议, 江苏·无锡
作者:  张少华;  李飞;  余西龙;  陈立红;  张新宇
Adobe PDF(433Kb)  |  收藏  |  浏览/下载：1007/228  |  提交时间：2010/11/25
Performance of the fuel injector in supersonic combustor 会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009
作者:  Wei Z(卫喆);  Chen LH(陈立红);  Gu HB(顾洪斌);  Li F(李飞);  Gu SL(顾声龙);  Chang XY(张新宇);  Wei, Z. (weizhejiji@yahoo.com.cn)
Adobe PDF(167Kb)  |  收藏  |  浏览/下载：174/59  |  提交时间：2017/07/14
Concentration Profiles  Engine Design  Fuel Injectors  Fuel-air Mixing  Gas Sampling  Ramp Injector  Scramjet Combustors  Scramjet Test  Supersonic Combustors  
A tunable diode-laser absorption spectroscopy (TDLAS) thermometry for combustion diagnostics 会议论文
15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, United states, April 28, 2008 - May 1, 2008
作者:  Yu XL(余西龙);  Li F(李飞);  Chen LH(陈立红);  Chang XY(张新宇)
Adobe PDF(265Kb)  |  收藏  |  浏览/下载：351/100  |  提交时间：2017/06/01
Absorption Lines  Combustion Diagnostics  Direct Absorption  Fiber-coupled  Flat Flame Burner  High Sensitivity  Near Infrared  Non-intrusive  Premixed  Scan Rates  Thermocouple Measurements  Tunable Diode Laser Absorption Spectroscopy  Tunable Diode Lasers  Water Vapor Concentration  Water-vapor Absorption  
Analyses of supersonic combustion by gas sampling 会议论文
13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference, Capua, Italy, May 16, 2005 - May 20, 2005
作者:  Chen LH(陈立红);  Lin R;  Gu HB(顾洪斌);  Chang XY(张新宇)
Adobe PDF(93Kb)  |  收藏  |  浏览/下载：198/82  |  提交时间：2017/06/01
Combustion Efficiency  Gas Sampling  Probe Sampling  Scramjet  
Combustion of kerosene in a supersonic stream 会议论文
38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, United states, January 10, 2000 - January 13, 2000
作者:  Li JG(李建国);  Yu G(俞刚);  Zhang XY(张新宇);  Huang QS
Adobe PDF(519Kb)  |  收藏  |  浏览/下载：179/95  |  提交时间：2017/06/01
Cavity Flame Holders  Combustion Efficiencies  Combustor Performance  Equivalence Ratios  Modular Structures  Optimized Conditions  Stagnation Pressures  Supersonic Combustors