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机构地区:[1]国防科技大学航天科学与工程学院,湖南长沙410073 [2]高超声速冲压发动机技术重点实验室,湖南长沙410073
出 处:《国防科技大学学报》2016年第2期48-55,共8页Journal of National University of Defense Technology
基 金:国家自然科学基金资助项目(11272351;11572346)
摘 要:采用大涡模拟数值计算二维空间发展的超声速混合层,重点分析横向扰动对混合层的标量结构、标量厚度以及标量体积卷吸率的影响。采用理论模型验证了数值方法在计算标量混合特性方面的准确性。结果表明,横向扰动频率和振幅明显影响着混合层的标量增长率和卷吸率。高频扰动增大了混合层近场标量增长率和卷吸率,但是低频扰动改善了混合层远场标量增长率。大尺度涡卷吸过程对混合层标量卷吸率起决定作用。多频扰动有效地增强了超声速混合层的标量混合。Numerical studies on a spatially developing supersonic mixing layer were performed by means of large-eddy simulation. Focusing on the effect of transverse forcing on the passive scalar mixing characteristic of mixing layer. The results for the baseline case without external forcing are in agreement with the analytical evidence. Afterwards, the effect of transverse forcing on the scalar structure, scalar thickness and volumetric entrainment ratio of mixing layer were analyzed. Results indicate that the frequency and amplitude of transverse forcing alter the growth rate and entrainment ratio of the passive scalar mixing significantly. High-frequency forcing magnifies the scalar thickness and volumetric entrainment ratio in the near field of mixing layer. However, the growth rate in the far field is increased by the low-frequency forcing. The entrainment ratio is, to be a large extent, dominated by the large-scale eddy entrainment process. The multiple-frequency forcing seems to validly enhance the scalar mixing in supersonic mixing layer.
关 键 词:横向扰动 超声速混合层 被动标量 动量比 卷吸率
分 类 号:V435.12[航空宇航科学与技术—航空宇航推进理论与工程]
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