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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)
浏览  |  Adobe PDF(265Kb)  |  收藏  |  浏览/下载：349/100  |  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  
Microgravity Smoldering Combustion Of Flexible Polyurethane Foam With Central Ignition 期刊论文
Microgravity Science And Technology, 2008, 页码: 99-105
作者:  Wang SF(王双峰);  Zhang X(张夏);  Wang, SF (reprint author), Chinese Acad Sci, Inst Mech, Natl Micrograv Lab, Beijing 100080, Peoples R China.
Adobe PDF(211Kb)  |  收藏  |  浏览/下载：738/169  |  提交时间：2009/08/03
Smoldering Combustion  Microgravity  Polyurethane Foam  Natural-convection  Propagation  Flow  
Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance 期刊论文
Combustion Science and Technology, 2007, 卷号: 179, 期号: 10, 页码: 2199-2217
作者:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Sung CJ;  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
Adobe PDF(1524Kb)  |  收藏  |  浏览/下载：845/231  |  提交时间：2009/08/03
Entry Conditions  Kerosene  Supersonic Combustion  Thermal Cracking  Model Combustor  Propulsion  Injection  
Determination of the Maximum Effective Burning Velocity of Dust-Air Mixtures in Constant Volume Combustion 期刊论文
JOURNAL OF LOSS PREVENTION IN THE PROCESS INDUSTRIES, 2007, 卷号: 20, 期号: 4-6, 页码: 462-469
作者:  Pu Y K;  Jia F;  Wang SF(王双峰);  Skjold T;  Pu, YK (reprint author), Chinese Acad Sci, Inst Mech, Natl Micrograv Lab, Beijing 100080, Peoples R China.
浏览  |  Adobe PDF(565Kb)  |  收藏  |  浏览/下载：257/85  |  提交时间：2016/01/11
Dust Explosion  Constant Volume Combustion  Maximum Effective Burning Velocity  
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)
浏览  |  Adobe PDF(93Kb)  |  收藏  |  浏览/下载：195/81  |  提交时间：2017/06/01
Combustion Efficiency  Gas Sampling  Probe Sampling  Scramjet  
Flow rate analyses and calibrations of kerosene cracking for supersonic combustion 会议论文
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ, United states, July 10, 2005 - July 13, 2005
作者:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国)
浏览  |  Adobe PDF(315Kb)  |  收藏  |  浏览/下载：229/60  |  提交时间：2017/06/01
Average Molecular Weight  Chemical Formulae  Cracking Model  Gaseous Products  High Temperature  Ideal Gas Law  Ideal Gas Mixtures  Mass Flow Rate  Mole Fraction  Residence Time  Room Temperature  Sonic Nozzle  Supercritical Condition  Supersonic Combustion  Temperature Dependencies  Thermal Cracking  Three-component  
Numerical Simulation of Nox Formation in Coal Combustion with Inlet Natural Gas Burning 期刊论文
Chinese Journal of Chemical Engineering, 2005, 卷号: 13, 期号: 3, 页码: 318-323
作者:  Zhang Y(张宇);  Zhou LX;  Wei XL(魏小林);  Sheng HZ(盛宏至);  Zhang, Y (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
浏览  |  Adobe PDF(422Kb)  |  收藏  |  浏览/下载：746/178  |  提交时间：2007/06/15
Coal Combustion  Natural Gas  Burning  Nox Formation  Numerical Simulation  
Development of the facility for model scramjet testing 会议论文
10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, Japan, April 24, 2001 - April 27, 2001
作者:  Chang XY(张新宇);  Chen LH(陈立红);  Yu G(俞刚);  Qian DX(钱大兴)
浏览  |  Adobe PDF(872Kb)  |  收藏  |  浏览/下载：212/80  |  提交时间：2017/06/01
Chinese Academy Of Sciences  Enthalpy Flow  Hypersonic Propulsion Test Facility  Performance Tests  Scramjet Testing  Supersonic Combustion  Total Pressure  Total Temperatures  
碳氢燃料超音速燃烧的数值研究 学位论文
硕士论文，北京: 中国科学院研究生院, 2000
作者:  沈月阳
Adobe PDF(8206Kb)  |  收藏  |  浏览/下载：436/1  |  提交时间：2009/04/13
横向喷射  六方程  化学反应  超音速燃烧  Ch_4  Tvd  Transverse Injection  Six Elementary Reactions  Chemical Reactions  Supersonic Combustion  
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
浏览  |  Adobe PDF(519Kb)  |  收藏  |  浏览/下载：174/92  |  提交时间：2017/06/01
Cavity Flame Holders  Combustion Efficiencies  Combustor Performance  Equivalence Ratios  Modular Structures  Optimized Conditions  Stagnation Pressures  Supersonic Combustors