Study on Flow Characteristic of Sub-/Super-Sonic Mixing Layer

In order to obtain the flow characteristics of sub-super-sonic mixing layer including velocity distribution, pressure distribution and development of mixing layer, experimental and numerical investigations were conducted. PIV technique was employed to measure the two-dimensional velocity distributio...

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Format: Article
Language:zho
Published: The Northwestern Polytechnical University 2020-06-01
Series:Xibei Gongye Daxue Xuebao
Subjects:
Online Access:https://www.jnwpu.org/articles/jnwpu/full_html/2020/03/jnwpu2020383p649/jnwpu2020383p649.html
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spelling doaj-1985c7494ffd4d9da49def7ce9ddab0c2021-05-02T18:10:15ZzhoThe Northwestern Polytechnical UniversityXibei Gongye Daxue Xuebao1000-27582609-71252020-06-0138364965610.1051/jnwpu/20203830649jnwpu2020383p649Study on Flow Characteristic of Sub-/Super-Sonic Mixing Layer01234College of Energy and Power Engineering, Nanjing University of Aeronautics and AstronauticsCollege of Energy and Power Engineering, Nanjing University of Aeronautics and AstronauticsCollege of Energy and Power Engineering, Nanjing University of Aeronautics and AstronauticsCollege of Energy and Power Engineering, Nanjing University of Aeronautics and AstronauticsCollege of Energy and Power Engineering, Nanjing University of Aeronautics and AstronauticsIn order to obtain the flow characteristics of sub-super-sonic mixing layer including velocity distribution, pressure distribution and development of mixing layer, experimental and numerical investigations were conducted. PIV technique was employed to measure the two-dimensional velocity distribution in the experiment while the standard k-ω turbulent considering the effect of compressibility was adopted to simulate the flow characteristic of mixing layer. The Mach number of subsonic stream and supersonic one was 0.11 and 1.32, respectively. The results show the flow of mixing layer is temporally transient. The interface between two streams lies initially as an approximately line segment; afterward, it becomes wrinkled and distorted; finally, it breaks up. The mixing layer develops linearly along streamwise direction in the time averaged velocity field with a growth rate of 0.135. The velocity and total pressure distributions in the mixing layer are self-similar.https://www.jnwpu.org/articles/jnwpu/full_html/2020/03/jnwpu2020383p649/jnwpu2020383p649.htmlmixing layerflow characteristicshear layergrowth rateself-similarsupersonic
collection DOAJ
language zho
format Article
sources DOAJ
title Study on Flow Characteristic of Sub-/Super-Sonic Mixing Layer
spellingShingle Study on Flow Characteristic of Sub-/Super-Sonic Mixing Layer
Xibei Gongye Daxue Xuebao
mixing layer
flow characteristic
shear layer
growth rate
self-similar
supersonic
title_short Study on Flow Characteristic of Sub-/Super-Sonic Mixing Layer
title_full Study on Flow Characteristic of Sub-/Super-Sonic Mixing Layer
title_fullStr Study on Flow Characteristic of Sub-/Super-Sonic Mixing Layer
title_full_unstemmed Study on Flow Characteristic of Sub-/Super-Sonic Mixing Layer
title_sort study on flow characteristic of sub-/super-sonic mixing layer
publisher The Northwestern Polytechnical University
series Xibei Gongye Daxue Xuebao
issn 1000-2758
2609-7125
publishDate 2020-06-01
description In order to obtain the flow characteristics of sub-super-sonic mixing layer including velocity distribution, pressure distribution and development of mixing layer, experimental and numerical investigations were conducted. PIV technique was employed to measure the two-dimensional velocity distribution in the experiment while the standard k-ω turbulent considering the effect of compressibility was adopted to simulate the flow characteristic of mixing layer. The Mach number of subsonic stream and supersonic one was 0.11 and 1.32, respectively. The results show the flow of mixing layer is temporally transient. The interface between two streams lies initially as an approximately line segment; afterward, it becomes wrinkled and distorted; finally, it breaks up. The mixing layer develops linearly along streamwise direction in the time averaged velocity field with a growth rate of 0.135. The velocity and total pressure distributions in the mixing layer are self-similar.
topic mixing layer
flow characteristic
shear layer
growth rate
self-similar
supersonic
url https://www.jnwpu.org/articles/jnwpu/full_html/2020/03/jnwpu2020383p649/jnwpu2020383p649.html
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