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A micro diffuser/nozzle pump with fins on the sidewall 会议论文
4th International Conference on Solid-State Sensors, Actuators and Microsystems, TRANSDUCERS and EUROSENSORS '07, Lyon, France, June 10, 2007 - June 14, 2007
作者:  Li XH;  Yu XM;  Zhang DC;  Li ZH;  Xu WH
浏览  |  Adobe PDF(402Kb)  |  收藏  |  浏览/下载：148/55  |  提交时间：2017/06/01
Diffuser/nozzle  Diffuser/nozzle Pump  Fins  Flow Efficiency  International Conferences  Key Parts  Novel Methods  Pump Performance  Silicon Micro-machining  Solid-state Sensors  
Performance of supersonic model combustors with distributed injection of supercritical kerosene 会议论文
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cincinnati, OH, United states, July 8, 2007 - July 11, 2007
作者:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Lu XN;  Sung CJ
Adobe PDF(423Kb)  |  收藏  |  浏览/下载：186/70  |  提交时间：2017/06/01
Stagnation Temperatures  Supercritical Kerosene  Supersonic Model Combustors  
Experimental investigation of cavity-based scramjet model 会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
作者:  Gu HB(顾洪斌);  Chen LH(陈立红);  张新宇(Chang XY)
浏览  |  Adobe PDF(162Kb)  |  收藏  |  浏览/下载：158/71  |  提交时间：2017/06/01
Kerosene Fuel  Mass Flow Rate  Scramjet Engine  
Wave Propagation Analysis in a Pressure-Wave-Refrigerator 会议论文
International Symposium on Physics of Fluids, JUN 09-12, 2005 Huangshan, PEOPLES R CHINA
作者:  Zhao W(赵伟);  Jiang ZL(姜宗林);  Yu HR(俞鸿儒);  Saito T;  Takayama K
Adobe PDF(438Kb)  |  收藏  |  浏览/下载：1033/301  |  提交时间：2007/12/18
Thrust and drag of a scramjet model with different combustor geometries 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:  Chang XY(张新宇);  Gu HB(顾洪斌);  Chen LH(陈立红)
浏览  |  Adobe PDF(139Kb)  |  收藏  |  浏览/下载：163/68  |  提交时间：2017/06/01
Combustor Geometries  Flame Stabilization  Mixing Enhancement  Scramjets  
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：198/82  |  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：233/60  |  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  
不同热化学模型对高超声速喷管流场影响的数值分析 会议论文
第十二届全国计算流体力学会议, 中国西安, 2004-8-1
作者:  曾明;  杭建;  林贞彬;  瞿章华
Adobe PDF(241Kb)  |  收藏  |  浏览/下载：314/137  |  提交时间：2014/02/14
高超声速流  喷管  热化学模型  非平衡  数值模拟  
Effects of Translational Nonequilibrium on Performance of Flowing Chemical Oxygen-Iodine Laser 会议论文
XIV International Symposium on Gas Flow, Chemical Lasers, and High-Power Lasers, 2003
作者:  Gao Z(高智);  Yan HX(严海星);  Hu LM(胡利民)
浏览  |  Adobe PDF(302Kb)  |  收藏  |  浏览/下载：553/125  |  提交时间：2007/06/15
Examination of the LBM in simulation of microchannel flow in transitional regime 会议论文
First International Conference on Microchannels and Minichannels, Rochester, NY, United states, April 24, 2003 - April 25, 2003
作者:  Shen Q(沈青);  Tian DB(田东波);  Xie C(谢翀);  Fan J(樊菁)
浏览  |  Adobe PDF(342Kb)  |  收藏  |  浏览/下载：321/161  |  提交时间：2017/06/01
Direct Simulation Monte Carlo (Dsmc) Method  Knudsen Number