Effect of Initial and Boundary Conditions on Development of Three-Dimensional Wall Jets

Pub Date : 2002-01-14 DOI:10.2514/6.2002-733
Hongguang Sun, D. Ewing
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Introduction The three-dimensional wall jet formed by a round jet exiting over a flat plate is an useful model for the wall jets that occur in many film cooling applications. One notable feature of these jets is the large anisotropy in the growth rate of the jet. The growth rate in the lateral direction is 'typically 4-6 times larger than that in the vertical direction. It is known that this large anisotropy in the growth rates is caused by the large-scale structures in the wall jet. Matsuda et al. 7 and Ewing and Pollard 5 recently proposed a model to explain how the vortex rings that develop in the jet shear layers deform to generate large-scale turbulent structures that cause the anisotropic growth rates. Abrahamsson et al. noted recently that there were significant differences in the reported growth rates for the three-dimensional wall jets. In particular, the lateral and vertical growth rates for the wall jet exiting a round contoured nozzle were approximately 15% and 20% larger than those of the jet exiting a round fully developed pipe. Eriksson et al. found that boundary conditions, such as the size or presence of a wall behind the jet exit could also affect the growth rate of the wall jet. Since different boundary conditions were used in many of previous measurements, it is not clear whether the differences of the growth rates observed by Abrahamsson et al. l are mainly Copyright© 2002 The American Institute of Aeronautics and Astronautics Inc. All rights reserved. caused by differences in initial conditions or boundary conditions. The objective of this investigation is to examine how changes in initial conditions and boundary conditions affect the development of three-dimensional wall jets. This was accomplished by performing a series of experiments where only one parameter was changed in each experiment. Initially, the effect of changes in initial conditions was investigated by examining the development of the flow exiting a contoured nozzle with top hat velocity profile and a long pipe with the fully developed velocity profile. Measurements were also performed for the wall jets with two different Reynolds numbers in the case of the fully developed pipe to examine if changes in Reynolds numbers affect the flow development. The effect of the wall behind the nozzle exit was then investigated by measuring the development of jets exiting fully developed pipe with and without this plate. Finally, the effect of changing the size of the back wall and in fact the room, was investigated by measuring the jet exiting a smaller fully developed pipe. In all cases, the development of the wall jet was characterized by measuring the profiles of the mean velocities and Reynolds stresses, and contours of the mean streamwise velocity and vorticity. The self-similar solutions for the three-dimensional wall jet outlined by Sun and Ewing 9 were used to scale the data. Initially the experimental facilities used in this experiment are described in detail. The key results of the similarity analysis outlined by Sun and Ewing 9 are summarized. Finally, the measurements for the different cases are presented and discussed. Experimental Facility and Procedures Measurements were performed in the wall jet exiting three different nozzles: a contoured nozzle, a large diameter long pipe, and a small diameter long pipe. In all cases, these jets exited tangentially to a horizontal plate with a length of 1.8 m and a width of 2.5 m shown in figure 1. The experimental apparatus was designed so a vertical wall could be positioned flush with the jet exit in order to block the entrainment from behind the jet. This wall had a width of 2.5 m and a height of 1.1 m. The first wall jet studied was formed from a jet exiting a contoured nozzle with an exit diameter of 38.1 mm. The contour on the inside nozzle was fifth order polynomial and the area contraction ratio was 28:1. The flow 1 American Institute of Aeronautics and Astronautics (c)2002 American Institute of Aeronautics & Astronautics or Published with Permission of Author(s) and/or Author(s)' Sponsoring Organization.","PeriodicalId":0,"journal":{"name":"","volume":" ","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2002-01-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"26","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.2514/6.2002-733","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 26

Abstract

Detailed flow field measurements in the wall jets exiting a contoured nozzle and two long pipes with different boundary conditions are reported here. It was found that the growth rate of the jets, the mean velocity and turbulence stress profiles, and the mean velocity and vorticity contours were essentially unaffected by the changes in exit conditions or initial conditions in the intermediate region. There were differences in the half-widths of the jets, the local Reynolds number and the decay of the velocity field downstream. It was also found that the presence of a wall behind the nozzle and the change of the size of this back wall and the room did not affect the jet spread in the lateral direction, but did affect the vertical width and growth rate. Introduction The three-dimensional wall jet formed by a round jet exiting over a flat plate is an useful model for the wall jets that occur in many film cooling applications. One notable feature of these jets is the large anisotropy in the growth rate of the jet. The growth rate in the lateral direction is 'typically 4-6 times larger than that in the vertical direction. It is known that this large anisotropy in the growth rates is caused by the large-scale structures in the wall jet. Matsuda et al. 7 and Ewing and Pollard 5 recently proposed a model to explain how the vortex rings that develop in the jet shear layers deform to generate large-scale turbulent structures that cause the anisotropic growth rates. Abrahamsson et al. noted recently that there were significant differences in the reported growth rates for the three-dimensional wall jets. In particular, the lateral and vertical growth rates for the wall jet exiting a round contoured nozzle were approximately 15% and 20% larger than those of the jet exiting a round fully developed pipe. Eriksson et al. found that boundary conditions, such as the size or presence of a wall behind the jet exit could also affect the growth rate of the wall jet. Since different boundary conditions were used in many of previous measurements, it is not clear whether the differences of the growth rates observed by Abrahamsson et al. l are mainly Copyright© 2002 The American Institute of Aeronautics and Astronautics Inc. All rights reserved. caused by differences in initial conditions or boundary conditions. The objective of this investigation is to examine how changes in initial conditions and boundary conditions affect the development of three-dimensional wall jets. This was accomplished by performing a series of experiments where only one parameter was changed in each experiment. Initially, the effect of changes in initial conditions was investigated by examining the development of the flow exiting a contoured nozzle with top hat velocity profile and a long pipe with the fully developed velocity profile. Measurements were also performed for the wall jets with two different Reynolds numbers in the case of the fully developed pipe to examine if changes in Reynolds numbers affect the flow development. The effect of the wall behind the nozzle exit was then investigated by measuring the development of jets exiting fully developed pipe with and without this plate. Finally, the effect of changing the size of the back wall and in fact the room, was investigated by measuring the jet exiting a smaller fully developed pipe. In all cases, the development of the wall jet was characterized by measuring the profiles of the mean velocities and Reynolds stresses, and contours of the mean streamwise velocity and vorticity. The self-similar solutions for the three-dimensional wall jet outlined by Sun and Ewing 9 were used to scale the data. Initially the experimental facilities used in this experiment are described in detail. The key results of the similarity analysis outlined by Sun and Ewing 9 are summarized. Finally, the measurements for the different cases are presented and discussed. Experimental Facility and Procedures Measurements were performed in the wall jet exiting three different nozzles: a contoured nozzle, a large diameter long pipe, and a small diameter long pipe. In all cases, these jets exited tangentially to a horizontal plate with a length of 1.8 m and a width of 2.5 m shown in figure 1. The experimental apparatus was designed so a vertical wall could be positioned flush with the jet exit in order to block the entrainment from behind the jet. This wall had a width of 2.5 m and a height of 1.1 m. The first wall jet studied was formed from a jet exiting a contoured nozzle with an exit diameter of 38.1 mm. The contour on the inside nozzle was fifth order polynomial and the area contraction ratio was 28:1. The flow 1 American Institute of Aeronautics and Astronautics (c)2002 American Institute of Aeronautics & Astronautics or Published with Permission of Author(s) and/or Author(s)' Sponsoring Organization.
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初始条件和边界条件对三维壁面射流发展的影响
本文报道了在不同边界条件下,从异形喷嘴和两根长管流出的壁面射流流场的详细测量结果。结果表明,射流的增长率、平均速度和湍流应力曲线以及平均速度和涡度曲线基本上不受中间区域出口条件或初始条件变化的影响。射流半宽、局部雷诺数和下游速度场衰减存在差异。研究还发现,喷嘴后壁的存在以及后壁和房间大小的变化并不影响射流在横向上的扩散,但确实影响了垂直宽度和生长速度。在许多薄膜冷却应用中,由圆形射流在平板上射出形成的三维壁面射流是一种有用的壁面射流模型。这些射流的一个显著特征是射流的生长速率具有很大的各向异性。横向生长速率通常是纵向生长速率的4-6倍。已知这种生长速率的大各向异性是由壁面射流中的大尺度结构引起的。Matsuda et al. 7和Ewing and Pollard 5最近提出了一个模型来解释在射流剪切层中发展的涡环如何变形以产生导致各向异性增长率的大规模湍流结构。Abrahamsson等人最近注意到,三维壁面射流的增长率在报道中存在显著差异。尤其值得一提的是,从圆形喷管流出的壁面射流的横向和垂直增长速率比从圆形管道流出的壁面射流的横向和垂直增长速率分别高出约15%和20%。Eriksson等人发现,边界条件,如射流出口后壁面的大小或存在与否,也会影响壁面射流的生长速度。由于在以前的许多测量中使用了不同的边界条件,因此尚不清楚Abrahamsson等人观察到的增长率差异是否主要是Copyright©2002 the American Institute of Aeronautics and Astronautics Inc.。版权所有。由初始条件或边界条件的差异引起的。本研究的目的是研究初始条件和边界条件的变化如何影响三维壁面射流的发展。这是通过进行一系列实验来完成的,每次实验只改变一个参数。首先,研究了初始条件变化的影响,通过检查具有高帽速度分布的轮廓喷嘴和具有充分发展速度分布的长管的流动发展。在完全打开的管道的情况下,还对两种不同雷诺数的壁面射流进行了测量,以检查雷诺数的变化是否会影响流动发展。然后通过测量带和不带该板的完全打开的管道的射流发展来研究喷嘴出口后壁的影响。最后,通过测量从一个更小的完全发育的管道流出的射流,研究了改变后壁(实际上是房间)尺寸的影响。在所有情况下,壁面射流的发展都是通过测量平均速度和雷诺应力的分布以及平均流向速度和涡量的轮廓来表征的。利用Sun和Ewing 9提出的三维壁面射流的自相似解对数据进行缩放。首先详细介绍了本实验所使用的实验设备。总结了Sun和Ewing 9提出的相似性分析的关键结果。最后,给出并讨论了不同情况下的测量结果。在三种不同喷嘴的壁面射流中进行了测量:一种是轮廓喷嘴,一种是大直径长管,一种是小直径长管。在所有情况下,这些射流都切向一个长1.8米、宽2.5米的水平板,如图1所示。实验装置被设计成与射流出口齐平的垂直壁,以阻止射流后面的夹带。这堵墙宽2.5米,高1.1米。所研究的第一个壁面射流是由出口直径为38.1 mm的异形喷嘴形成的。喷嘴内轮廓为五阶多项式,面积收缩比为28:1。流1美国航空航天研究所(c)2002年美国航空航天研究所或出版与作者(s)和/或作者(s)赞助组织的许可。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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