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高雷诺数超声速混合层标量输运与扩散特性研究进展
引用本文:沈赤兵,石少平,冯军红.高雷诺数超声速混合层标量输运与扩散特性研究进展[J].国防科技大学学报,2016,38(4):164-173.
作者姓名:沈赤兵  石少平  冯军红
作者单位:国防科技大学航天科学与工程学院,国防科技大学训练部,国防科技大学航天科学与工程学院
基金项目:国家自然科学基金项目(面上项目,重点项目,重大项目)(编号:11572346)
摘    要:围绕超声速混合层标量混合在组合循环发动机中的应用,综述了超声速混合层以及超声速混合层标量混合过程的国内外研究进展,并针对高雷诺数超声速混合层标量输运与扩散特性研究中存在的不足提出解决办法,指出该领域值得深入开展的研究方向。

关 键 词:组合循环发动机  超声速混合层  标量混合  雷诺数  强化混合
收稿时间:2015/10/9 0:00:00

Scalar transport and diffusion study progress of supersonic mixing layer with high Reynolds number
SHEN Chibing,SHI Shaoping and FENG Junhong.Scalar transport and diffusion study progress of supersonic mixing layer with high Reynolds number[J].Journal of National University of Defense Technology,2016,38(4):164-173.
Authors:SHEN Chibing  SHI Shaoping and FENG Junhong
Institution:SHEN Chibing;SHI Shaoping;FENG Junhong;College of Aerospace Science and Engineering,National University of Defense Technology;Science and Technology on Scramjet Laboratory,National University of Defense Technology;Training Department,National University of Defense Technology;
Abstract:The mixing processes of fuel-rich gas and air in the combustor of combined cycle engine was viewed as the supersonic mixing layer which was featured by the high Reynolds number. Moreover, the transport and diffusion processes of scalars including temperature and concentration were important factors for controlling the gas-gas mixing and combustion process. Under high Reynolds number, the turbulence scale, the transport and diffusion of scalar, vortex shape and scalar interfacial area of the mixing flow field revealed more complex physical mechanisms. In this paper, the application background of the scalar mixing in the supersonic mixing layer on the combined cycle engine was introduced, and the study progress of the supersonic mixing layer and the scalar mixing process in the supersonic mixing layer both at home and abroad was summarized, then the methods for counteracting the shortcomings of the study on scalar transport and diffusion characteristics of supersonic mixing layer with high Reynolds number were proposed. Finally, some directions being worth studying deeply in the field were pointed out.
Keywords:combined cycle engine  supersonic mixing layer  scalar mixing  Reynolds number  intensifying mixing  
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