Effect of uniform blowing or suction on hypersonic spatially developing turbulent boundary layers
查看参考文献8篇
文摘
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Over the past decades, the reduction of drag has attracted considerable attention for its potential applications in engineering [1-3]. Direct numerical simulations (DNSs) provide accurate data that can be used to study the underlying physics of drag reduction. In a recent DNS [4] of an incompressible spatially developing turbulent boundary layer with uniform blowing or suction applied on the wall, the drag reduction mechanism was quantitatively explained by the Fukagata, Iwamoto and Kasagi (FIK) identity [5]. Compared with incompressible flows, far fewer studies have been reported for high-speed (hypersonic) flows. Therefore, the purpose of this study is to investigate the effects of uniform blowing and uniform suction on the skin-friction in hypersonic turbulent boundary layers. |
来源
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Science China. Physics
, Mechanics & Astronomy,2016,59(6):664702-1-664702-2 【核心库】
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DOI
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10.1007/s11433-015-0511-0
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地址
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Institute of Mechanics, Key Laboratory of High Temperature Gas Dynamics, Chinese Academy of Sciences, Beijing, 100190
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语种
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英文 |
文献类型
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研究性论文 |
ISSN
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1674-7348 |
学科
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力学 |
基金
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国家自然科学基金
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国家973计划
;
the Chinese Academy of Sciences Program
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文献收藏号
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CSCD:5712916
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参考文献 共
8
共1页
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