IMECH-IR

Browse/Search Results:  1-6 of 6 Help

Filters                    
Selected(0)Clear Items/Page:    Sort:
低中功率氢电弧加热发动机内传热与流动特性比较研究 会议论文
2011中国工程热物理学会学术会议, 西安, 2011-10
Authors:  魏福智;  王海兴;  陈熙;  潘文霞
Adobe PDF(853Kb)  |  Favorite  |  View/Download:1051/293  |  Submit date:2012/01/06
电弧加热发动机  数值模拟  低中功率  传热与流动  
Experimental study on energy dissipation in a 1 kW arcjet thruster 会议论文
13th Asian Congress of Fluid Mechanics, Dhaka, Bangladesh, 2010-12-17~2010-12-21
Authors:  Huang HJ(黄河激);  Pan WX(潘文霞);  Wu CK(吴承康)
Adobe PDF(255Kb)  |  Favorite  |  View/Download:773/204  |  Submit date:2011/01/12
Arcjet Thruster  Performance  Energy Dissipation  
Volt-ampere characteristics, nozzle temperature and thruster performances in a low power argon arcjet 会议论文
13th Asian Congress of Fluid Mechanics, Dhaka, Bangladesh, 2010-12-17~2010-12-21
Authors:  Pan WX(潘文霞);  Meng X(孟显);  Wu CK(吴承康)
Adobe PDF(139Kb)  |  Favorite  |  View/Download:1239/335  |  Submit date:2011/01/12
eywor Arcjet Thruster  volt-ampere Characteristics  Nozzle Temperature  
低功率电弧加热推力器喷管温度与性能 会议论文
第6届中国电推进技术学术研讨会论文集, 北京, 2010-09-02~2010-09-03
Authors:  潘文霞;  黄河激;  孟显;  吴承康
Adobe PDF(745Kb)  |  Favorite  |  View/Download:1010/288  |  Submit date:2011/01/12
电弧加热推力器  喷管温升  电弧特性  性能变化  
Experimental study on energy dissipation in a 1 kW arcjet thruster 会议论文
13th Asian Congress of Fluid Mechanics, Dhaka, Bangladesh, 2010-11-17~2010-11-21
Authors:  Huang HJ(黄河激);  Pan WX(潘文霞);  Wu CK(吴承康)
Adobe PDF(255Kb)  |  Favorite  |  View/Download:797/248  |  Submit date:2011/01/06
 arcjet Thruster  Performance  Energy dissipation  
Effects of anode temperature on the arc volt-ampere characteristics and ejected plume property of a low-power supersonic plasma 期刊论文
Plasma Sources Science & Technology, 2011, 卷号: 20, 期号: 6, 页码: 65006
Authors:  Pan WX(潘文霞);  Meng X(孟显);  Huang HJ(黄河激);  Wu CK(吴承康);  Pan, WX, Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China
Adobe PDF(463Kb)  |  Favorite  |  View/Download:1217/252  |  Submit date:2012/03/31
Performance  Deposition  Nitrogen  Thruster  Surface  Argon