A method of mixing process control in a shear layer of a supersonic nonisobaric jet

机译：一种超音速非等压射流剪切层内混合过程控制的方法

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A possibility of ocntrolling the process of mixing in the shear of the initial section of a supersonic nonisobaric jet is based on the relatively discovered new physical phenomenon connected with the formation of stationary streamwise vortex structures at the boundary of a supersonic underexpanded jet.

机译：在超音速非等压射流初始截面的剪切中控制混合过程的可能性是基于相对发现的新的物理现象，该现象与在超音速超膨胀射流边界处形成的固定流向涡旋结构有关。

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来源
《Mechanics of passive and active flow control》|1998年|p.101-108|共8页
会议地点 Gottingen(DE)
作者
V.I.Zapryagaev;
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原文格式 PDF
正文语种 eng
中图分类力学;
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机译：RAN / ILES方法的使用来研究COFLOW风对热，无异构，超声波氧化机射流流动的影响，在其与喷射爆破偏转器的相互作用期间
2. Large eddy simulation on using a cavity-jet controller for supersonic blunt base mixing layer control [J] . Zhou Yong-yi, Yang Rui, Zhao Yu-xin Acta astronautica . 2019,第AUGa期

机译：使用腔喷射控制器进行超声速钝基混合层控制的大涡模拟
3. Large eddy simulation on using a cavity-jet controller for supersonic blunt base mixing layer control [J] . Zhou Yong-yi, Yang Rui, Zhao Yu-xin Acta astronautica . 2019,第Auga期

机译：用于超声波钝基部混合层控制的腔 - 喷射控制器的大型涡流仿真
4. A method of mixing process control in a shear layer of a supersonic nonisobaric jet [C] . V.I.Zapryagaev IUTAM symposium on mechanics of passive and active flow control . 1999

机译：一种在超声波非异常射流剪切层中混合过程控制的方法
5. Mixing enhancement in supersonic compressible shear layers. [D] . Lee, Long-Shin. 1996

机译：超音速可压缩剪切层的混合增强。
6. Assessment of transvalvular flow jet angle in aortic dilation patients using 4D flow jet shear layer detection method [O] . Julio Garcia, Michael Markl, Pim van Ooij, 2014

机译：使用4D射流剪切层检测方法评估主动脉扩张患者的瓣膜射流角度。
7. Instabilities of Confined, Supersonic, Double Shear Layer Flow. A candidate mixing enhancement scheme in two-dimensional flow configuration. [O] . Akira UMEMURA, Yoichi TAKIHANA 1997

机译：限制，超音速，双剪切层流动的稳定性。二维流动配置中的候选混合增强方案。
8. Mixing of Supersonic Jets Including the Effects of Supersonic Jets Including the Effects of Transverse Pressure Gradient Using Difference Methods [R] . Kurkov, A. P. 1971

机译：超音速喷射混合包括超音速喷射的影响包括横向压力梯度的影响差异方法

A method of mixing process control in a shear layer of a supersonic nonisobaric jet

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