Instabilities in high Reynolds number flows

An asymptotic method for predicting stability characteristics, both stationary and travelling crossflow vortices, over a variety of surface variations was created. These include flat, convex and concave curved surfaces. Comparisons were made with two different numerical methods (Parabolised Stabilit...

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Main Author: Banks, Curtis Alwyn
Other Authors: Hall, Philip
Published: Imperial College London 2015
Subjects:
510
Online Access:http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.679678
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spelling ndltd-bl.uk-oai-ethos.bl.uk-6796782016-08-04T03:44:09ZInstabilities in high Reynolds number flowsBanks, Curtis AlwynHall, Philip2015An asymptotic method for predicting stability characteristics, both stationary and travelling crossflow vortices, over a variety of surface variations was created. These include flat, convex and concave curved surfaces. Comparisons were made with two different numerical methods (Parabolised Stability Equations and Velocity-Vorticity) and good agreement, to within 5% of the numerical value of the crossflow mode streamwise growth rate was met for both stationary and travelling modes initially for a flat surface. An additional comparison was made with the streamwise growth rates to observe the impact of including curvature and a small convex curvature surface variation was used. Similar results were achieved for this study also. Likewise results for travelling crossflow modes were with accordance with the numerical values. To understand how effective this disturbance in penetrating the boundary-layer, receptivity analysis was developed to analyse various mechanisms in the production of crossflow vortices. A response function was established from the receptivity analysis to calculate the efficiency of this process. The response function is largest near the leading edge, meaning the disturbance is most effective at propagating into the boundary layer there. This means that the approach qualitatively agrees with other research methods. This is true for all surface curvatures and both crossflow modes. There is an intriguing behaviour the response function exhibits for small concave curvature with travelling modes at a moderate frequency. When we consider moderate spanwise wavenumber, the response function is much larger than other modes or surface variation and this could have repercussions for experiments. Careful consideration is needed for this case and can be avoided with the aid of this research. Finally, an asymptotic theory was created to analyse two-dimensional closed streamlines for secondary instabilities. The first instability analysed was the elliptical instability, due to the links to turbulence and the initial interest in this general problem. The method anticipates the existence of short-wave three-dimensional disturbances on a streamline at a distance away from the centre of the vortex of this secondary instability. There was no limitation in the study for symmetrical known streamlines, the analysis can be extended further to analyse any two-dimensional closed streamline such as separation bubbles. With this in mind an observation was required to test this hypothesis and the approach was tested on the structure inside a cavity, from which the location and behaviour of the disturbance was correctly predicted.510Imperial College Londonhttp://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.679678http://hdl.handle.net/10044/1/29416Electronic Thesis or Dissertation
collection NDLTD
sources NDLTD
topic 510
spellingShingle 510
Banks, Curtis Alwyn
Instabilities in high Reynolds number flows
description An asymptotic method for predicting stability characteristics, both stationary and travelling crossflow vortices, over a variety of surface variations was created. These include flat, convex and concave curved surfaces. Comparisons were made with two different numerical methods (Parabolised Stability Equations and Velocity-Vorticity) and good agreement, to within 5% of the numerical value of the crossflow mode streamwise growth rate was met for both stationary and travelling modes initially for a flat surface. An additional comparison was made with the streamwise growth rates to observe the impact of including curvature and a small convex curvature surface variation was used. Similar results were achieved for this study also. Likewise results for travelling crossflow modes were with accordance with the numerical values. To understand how effective this disturbance in penetrating the boundary-layer, receptivity analysis was developed to analyse various mechanisms in the production of crossflow vortices. A response function was established from the receptivity analysis to calculate the efficiency of this process. The response function is largest near the leading edge, meaning the disturbance is most effective at propagating into the boundary layer there. This means that the approach qualitatively agrees with other research methods. This is true for all surface curvatures and both crossflow modes. There is an intriguing behaviour the response function exhibits for small concave curvature with travelling modes at a moderate frequency. When we consider moderate spanwise wavenumber, the response function is much larger than other modes or surface variation and this could have repercussions for experiments. Careful consideration is needed for this case and can be avoided with the aid of this research. Finally, an asymptotic theory was created to analyse two-dimensional closed streamlines for secondary instabilities. The first instability analysed was the elliptical instability, due to the links to turbulence and the initial interest in this general problem. The method anticipates the existence of short-wave three-dimensional disturbances on a streamline at a distance away from the centre of the vortex of this secondary instability. There was no limitation in the study for symmetrical known streamlines, the analysis can be extended further to analyse any two-dimensional closed streamline such as separation bubbles. With this in mind an observation was required to test this hypothesis and the approach was tested on the structure inside a cavity, from which the location and behaviour of the disturbance was correctly predicted.
author2 Hall, Philip
author_facet Hall, Philip
Banks, Curtis Alwyn
author Banks, Curtis Alwyn
author_sort Banks, Curtis Alwyn
title Instabilities in high Reynolds number flows
title_short Instabilities in high Reynolds number flows
title_full Instabilities in high Reynolds number flows
title_fullStr Instabilities in high Reynolds number flows
title_full_unstemmed Instabilities in high Reynolds number flows
title_sort instabilities in high reynolds number flows
publisher Imperial College London
publishDate 2015
url http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.679678
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