Single Jet Impingement Cooling in a Stationary and Rotating Square Duct

博士 === 國立中山大學 === 機械與機電工程學系研究所 === 91 === Abstract The influence of rotating and cross flow effect on local heat transfer coefficient and flow visualization for a single confined air/water jet with jet-to-wall spacing from 5 to 11.4, jet Reynolds number from 6500 to 26000, rotational Reynolds numbe...

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Main Authors: Jung-Tai Huang, 黃榮泰
Other Authors: Shou-Shing Hsieh
Format: Others
Language:zh-TW
Published: 2003
Online Access:http://ndltd.ncl.edu.tw/handle/99874953445579808196
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spelling ndltd-TW-091NSYS54900702016-06-22T04:20:47Z http://ndltd.ncl.edu.tw/handle/99874953445579808196 Single Jet Impingement Cooling in a Stationary and Rotating Square Duct 單噴流於靜止及旋轉通道內衝擊冷卻現象研究 Jung-Tai Huang 黃榮泰 博士 國立中山大學 機械與機電工程學系研究所 91 Abstract The influence of rotating and cross flow effect on local heat transfer coefficient and flow visualization for a single confined air/water jet with jet-to-wall spacing from 5 to 11.4, jet Reynolds number from 6500 to 26000, rotational Reynolds number from 0 to 112000, curvature ratio from 150 to , ratio of crossflow massflux to jet mass flux from 0 to 2, and the heat flux from 1430 to 12890W/m2 were reported. The local heat transfer coefficient for air/water along the surface is measured and the effect of the rotation, the jet-to-wall spacing, the surface curvature, local and average Nusselt number, are presented and discussed. Furthermore, flow visualization was made in the present study. Based on the experimental result, it is found that the rotation will induce the centrifugal and coriolis force. It also shows that the heat transfer response will be decreased when the impinging direction parallel to the rotating direction, and increased when impinging direction perpendicular to the rotating direction. Crossflow effect will make Nusselt number decrease to 48% when M=2. Moreover, the roughen surface will increase the heat transfer coefficient up to 22% due to the secondary flow. The flow visualization is used to observe the transition of laminar to turbulence flow and to calculate the boundary layer thickness. Shou-Shing Hsieh 謝曉星 2003 學位論文 ; thesis 185 zh-TW
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language zh-TW
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description 博士 === 國立中山大學 === 機械與機電工程學系研究所 === 91 === Abstract The influence of rotating and cross flow effect on local heat transfer coefficient and flow visualization for a single confined air/water jet with jet-to-wall spacing from 5 to 11.4, jet Reynolds number from 6500 to 26000, rotational Reynolds number from 0 to 112000, curvature ratio from 150 to , ratio of crossflow massflux to jet mass flux from 0 to 2, and the heat flux from 1430 to 12890W/m2 were reported. The local heat transfer coefficient for air/water along the surface is measured and the effect of the rotation, the jet-to-wall spacing, the surface curvature, local and average Nusselt number, are presented and discussed. Furthermore, flow visualization was made in the present study. Based on the experimental result, it is found that the rotation will induce the centrifugal and coriolis force. It also shows that the heat transfer response will be decreased when the impinging direction parallel to the rotating direction, and increased when impinging direction perpendicular to the rotating direction. Crossflow effect will make Nusselt number decrease to 48% when M=2. Moreover, the roughen surface will increase the heat transfer coefficient up to 22% due to the secondary flow. The flow visualization is used to observe the transition of laminar to turbulence flow and to calculate the boundary layer thickness.
author2 Shou-Shing Hsieh
author_facet Shou-Shing Hsieh
Jung-Tai Huang
黃榮泰
author Jung-Tai Huang
黃榮泰
spellingShingle Jung-Tai Huang
黃榮泰
Single Jet Impingement Cooling in a Stationary and Rotating Square Duct
author_sort Jung-Tai Huang
title Single Jet Impingement Cooling in a Stationary and Rotating Square Duct
title_short Single Jet Impingement Cooling in a Stationary and Rotating Square Duct
title_full Single Jet Impingement Cooling in a Stationary and Rotating Square Duct
title_fullStr Single Jet Impingement Cooling in a Stationary and Rotating Square Duct
title_full_unstemmed Single Jet Impingement Cooling in a Stationary and Rotating Square Duct
title_sort single jet impingement cooling in a stationary and rotating square duct
publishDate 2003
url http://ndltd.ncl.edu.tw/handle/99874953445579808196
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