Effect of wall confinement on the aerodynamics of bluff bodies

The effect of wall confinement on the aerodynamics of a set of stationary circular cylinders and flat plates, representing the blockage ratio range of 3 - 35.5%, is investigated experimentally to obtain data on mean and unsteady pressure distributions, Strouhal number, and wake geometry. In general,...

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Main Author: El-Sherbiny, Saad el-Sayed
Language:English
Published: University of British Columbia 2011
Online Access:http://hdl.handle.net/2429/32541
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spelling ndltd-UBC-oai-circle.library.ubc.ca-2429-325412018-01-05T17:46:43Z Effect of wall confinement on the aerodynamics of bluff bodies El-Sherbiny, Saad el-Sayed The effect of wall confinement on the aerodynamics of a set of stationary circular cylinders and flat plates, representing the blockage ratio range of 3 - 35.5%, is investigated experimentally to obtain data on mean and unsteady pressure distributions, Strouhal number, and wake geometry. In general, the influence of the Reynolds number in the range of 10⁴ -12 x 10⁴ was found to be confined to the mean pressure distribution at the higher blockage (circular cylinder only) and the unsteady surface loading. The results showed the base pressure to decrease and consequently the drag coefficient to increase with bluffness; however, the pressure distribution in the potential flow region remained relatively unaffected by the confinement. The wake geometry does not change appreciably under constraint and thus leads to a similarity of the several flow parameters. Variation in the vortex shedding frequency was found to be essentially proportional to the increase of separation velocity in accordance with Roshko's universal Strouhal number. The shape of the fluctuating surface pressure distribution curves also remains unaffected by the constraint. However, the pressure intensity increases with an increase in bluffness and shows considerable dependence on the Reynolds number and the three-dimensionality of the flow. Validity of the correction methods due to Glauert and Maskell for the mean drag coefficient is checked in the light of the experimental results. They were found to be inadequate particularly at higher blockage ratios. However, modification of these methods through inclusion of the higher order terms improved their applicability. Least square fit of the results showed linear variation [e.g., C[sub D] = C[sub D[sub c]] + Const (C[sub D] S/C)] of the parameters. A potential flow model is developed for two-dimensional symmetrical bluff bodies under wall confinement. It provides a procedure for predicting the mean surface loading on a bluff body over a range of blockage ratios. Experimental results with normal flat plates and circular cylinders for blockage ratios up to 35.5% substantiate the validity of the approach. Applied Science, Faculty of Mechanical Engineering, Department of Graduate 2011-03-17T19:03:30Z 2011-03-17T19:03:30Z 1972 Text Thesis/Dissertation http://hdl.handle.net/2429/32541 eng For non-commercial purposes only, such as research, private study and education. Additional conditions apply, see Terms of Use https://open.library.ubc.ca/terms_of_use. University of British Columbia
collection NDLTD
language English
sources NDLTD
description The effect of wall confinement on the aerodynamics of a set of stationary circular cylinders and flat plates, representing the blockage ratio range of 3 - 35.5%, is investigated experimentally to obtain data on mean and unsteady pressure distributions, Strouhal number, and wake geometry. In general, the influence of the Reynolds number in the range of 10⁴ -12 x 10⁴ was found to be confined to the mean pressure distribution at the higher blockage (circular cylinder only) and the unsteady surface loading. The results showed the base pressure to decrease and consequently the drag coefficient to increase with bluffness; however, the pressure distribution in the potential flow region remained relatively unaffected by the confinement. The wake geometry does not change appreciably under constraint and thus leads to a similarity of the several flow parameters. Variation in the vortex shedding frequency was found to be essentially proportional to the increase of separation velocity in accordance with Roshko's universal Strouhal number. The shape of the fluctuating surface pressure distribution curves also remains unaffected by the constraint. However, the pressure intensity increases with an increase in bluffness and shows considerable dependence on the Reynolds number and the three-dimensionality of the flow. Validity of the correction methods due to Glauert and Maskell for the mean drag coefficient is checked in the light of the experimental results. They were found to be inadequate particularly at higher blockage ratios. However, modification of these methods through inclusion of the higher order terms improved their applicability. Least square fit of the results showed linear variation [e.g., C[sub D] = C[sub D[sub c]] + Const (C[sub D] S/C)] of the parameters. A potential flow model is developed for two-dimensional symmetrical bluff bodies under wall confinement. It provides a procedure for predicting the mean surface loading on a bluff body over a range of blockage ratios. Experimental results with normal flat plates and circular cylinders for blockage ratios up to 35.5% substantiate the validity of the approach. === Applied Science, Faculty of === Mechanical Engineering, Department of === Graduate
author El-Sherbiny, Saad el-Sayed
spellingShingle El-Sherbiny, Saad el-Sayed
Effect of wall confinement on the aerodynamics of bluff bodies
author_facet El-Sherbiny, Saad el-Sayed
author_sort El-Sherbiny, Saad el-Sayed
title Effect of wall confinement on the aerodynamics of bluff bodies
title_short Effect of wall confinement on the aerodynamics of bluff bodies
title_full Effect of wall confinement on the aerodynamics of bluff bodies
title_fullStr Effect of wall confinement on the aerodynamics of bluff bodies
title_full_unstemmed Effect of wall confinement on the aerodynamics of bluff bodies
title_sort effect of wall confinement on the aerodynamics of bluff bodies
publisher University of British Columbia
publishDate 2011
url http://hdl.handle.net/2429/32541
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