| Citation: | YANG Min, CHANG Hai-ping, WU Pei-guang. Experimental study of heat transfer effect of a new cooling technique based on thermally driven theory[J]. Journal of Aerospace Power, 2006, 21(6): 989-994.
|
| [1] |
常海萍,过增元.一种燃气涡轮冷却叶片[P].实用新型专利,专利号:ZL 01217525.0Chang Hai-ping,Guo Zeng-yuan.A new technique used in turbine blade[P].Invention Patent,NO:ZL 01217525.
|
| [2] |
毛军逵,常海萍.一种新型冷却循环通道内水的热驱动数值分析[J].南京航空航天大学学报,2002,34(6):522-526.Mao Jun-kui,Chang Hai-ping.Simulation of thermal driving water in circular region used in high power density electronic systems[J].Journal of NUAA,2002,34(6):522-526.
|
| [3] |
毛军逵,常海萍,方立.离心力场下细微封闭通道内R12的热驱动换热研究[J].航空动力学报,2003,18(4):498-501.Mao Jun-kui,Chang Hai-ping,Fang Li.Experimental investigation of flow and heat transfer about the thermal driving of R12 in rotating small-size circular enclosures[J].Journal of Aerospace Power,2003,18(4):498-501.
|
| [4] |
毛军逵,常海萍,方立.离心力场流体热驱动液晶显现实验研究[J].工程热物理学报,2004,25(2):229-231.Mao Jun-kui,Chang Hai-ping,Fang Li.Investigation of thermal driving in centrifugal field with liquid crystal[J].Journal of Enginee-ring Thermophysics,2004,25(2):229-231.
|
| [5] |
杨敏,常海萍,毛军逵.离心力场下H2O和R12热驱动换热特性实验研究[J].工程热物理学报,2004,25(2):302-304.Yang Min,Chang Hai-ping,Mao Jun-kui.Experimental investigation of thermally driving heat transfer characteristics of H2O and R12 in a centrifugal force field[J].Journal of Engineering Thermophysics,2004,25(2):302-304.
|
| [6] |
杨敏,常海萍,毛军逵,等.离心力场下热驱动换热准则关系式的确定[J].航空动力学报,2005,20(3):467～471.Yang Min,Chang Hai-ping,Mao Jun-kui,et al.Determination of the similarity criteria for thermally driven heat transfer in centrifugal force field[J].Journal of Aerospace Power,2005,20(3):467-471.
|
| [7] |
Obot N T,Trabold T A.Impingement heat transfer with in arrays of circular jets:Part 1 -Effects of minimum,intermediate and complete crossflow for small and large spacing[J].Transactions of the ASME,1987,109:872～879.
|
| [8] |
张净玉,常海萍.冲击粗糙壁面复合冷却实验研究[J].航空动力学报,2001,16(4):386-389.Zhang Jing-yu,Chang Hai-ping.Experimental investigation on impinge-ment heat transfer from rib roughened surface[J].Journal of Aerospace Power,2001,16(4):386-389.
|
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