国防科技大学学报2016，Vol.38Issue(4)：164-173,10.DOI:10.11887/j.cn.201604026
高雷诺数超声速混合层标量输运与扩散特性研究进展
Scalar transport and diffusion study progress of supersonic mixing layer with high Reynolds number
摘要
Abstract
For the problem of the application of the scalar mixing of supersonic mixing layer in the combined cycle engine,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.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Key words
combined cycle engine/supersonic mixing layer/scalar mixing/Reynolds number/intensifying mixing分类
航空航天引用本文复制引用
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):164-173,10.基金项目
国家自然科学基金资助项目 （）
