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Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
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Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(832Kb)  |  收藏  |  浏览/下载:274/81  |  提交时间:2018/11/08
Combustion  Cost benefit analysis  Costs  Mixtures  Ramjet engines  Supersonic aircraft  Computational costs  Equivalence ratios  Local flow conditions  Scramjet combustors  Statistics approaches  Supersonic combustion  Supersonic combustors  Turbulent combustion  
Plasma Assisted Low Temperature Combustion 会议论文
22nd International Symposium on Plasma Chemistry (ISPC 22), Antwerp, BELGIUM, JUL 05-10, 2015
作者:  Ju YG;  Lefkowitz JK;  Reuter CB;  Won SH;  Yang XL;  Yang S;  Sun WT;  Jiang ZL(姜宗林);  Chen Q;  Ju, YG (reprint author), Princeton Univ, Dept Mech & Aerosp Engn, Princeton, NJ 08544 USA.
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Plasma Assisted Combustion  Low Temperature Chemistry  Kinetics  Cool Flames  S-curve Transition  Nonequilibrium Plasma  Saturated-hydrocarbons  Diffusion Flames  Pulsed Discharge  Ignition  Mixtures  Oxidation  Kinetics  Enhancement  
Experimental study of erosion threshold of reconstituted sediments 会议论文
30th International Conference on Ocean, Offshore and Arctic Engineering, Rotterdam, NETHERLANDS, JUN 19-24, 2011
作者:  Ye ZH;  Cheng L;  Zang ZP(臧志鹏);  Ye, ZH (reprint author), Univ Western Australia, Sch Civil & Resource Engn, Perth, WA 6009, Australia.
Adobe PDF(2495Kb)  |  收藏  |  浏览/下载:803/169  |  提交时间:2013/02/26
Arctic Engineering  Erosion  Mixtures  Sedimentology  Shear Stress  Coarse Particles  Cohesive Sediments  Equilibrium Modes  Erosion Characteristics  Erosion Thresholds  Experimental Studies  Mass Content  Mud Weights  Natural Sediments  Predicting Models  Research Efforts  Seabed Sediments  Test Condition  Testing Facility  
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)
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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