Compressible Flow Calculations of the Internal Flow Field for U- and V-shaped Air-Jet Texturing Nozzles

碩士 === 中原大學 === 機械工程研究所 === 95 === In order to investigate the internal flow characteristics of air-jet nozzles, a numerical approach is employed in this study. Based on a steady flow assumption and neglecting the influences of gravity, viscosity and yarn, the inviscid, compressible flow calculation...

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Main Authors: Jian-Tang Huang, 黃建棠
Other Authors: Shiu-Wu Chau
Format: Others
Language:zh-TW
Published: 2007
Online Access:http://ndltd.ncl.edu.tw/handle/89057676895991652695
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spelling ndltd-TW-095CYCU54890552015-10-13T13:56:23Z http://ndltd.ncl.edu.tw/handle/89057676895991652695 Compressible Flow Calculations of the Internal Flow Field for U- and V-shaped Air-Jet Texturing Nozzles U型與V型空氣噴嘴內部可壓縮流場計算分析研究 Jian-Tang Huang 黃建棠 碩士 中原大學 機械工程研究所 95 In order to investigate the internal flow characteristics of air-jet nozzles, a numerical approach is employed in this study. Based on a steady flow assumption and neglecting the influences of gravity, viscosity and yarn, the inviscid, compressible flow calculations are conducted for the internal flow passage of U- and V-type air-jet nozzles, where the air is assumed following the ideal gas law. The governing equations are discretized by a finite volume approach, where the first-order upwind scheme is employed to approximate the convection term in the governing equations. A SIMPLE-type algorithm is adopted to decouple the velocity and pressure in the flow fields. Available experiment measurements are then used to validate the numerical simulations. Keywords: air-Jet nozzle, compressible flow calculation, computational fluid dynamics. Shiu-Wu Chau 趙修武 2007 學位論文 ; thesis 86 zh-TW
collection NDLTD
language zh-TW
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description 碩士 === 中原大學 === 機械工程研究所 === 95 === In order to investigate the internal flow characteristics of air-jet nozzles, a numerical approach is employed in this study. Based on a steady flow assumption and neglecting the influences of gravity, viscosity and yarn, the inviscid, compressible flow calculations are conducted for the internal flow passage of U- and V-type air-jet nozzles, where the air is assumed following the ideal gas law. The governing equations are discretized by a finite volume approach, where the first-order upwind scheme is employed to approximate the convection term in the governing equations. A SIMPLE-type algorithm is adopted to decouple the velocity and pressure in the flow fields. Available experiment measurements are then used to validate the numerical simulations. Keywords: air-Jet nozzle, compressible flow calculation, computational fluid dynamics.
author2 Shiu-Wu Chau
author_facet Shiu-Wu Chau
Jian-Tang Huang
黃建棠
author Jian-Tang Huang
黃建棠
spellingShingle Jian-Tang Huang
黃建棠
Compressible Flow Calculations of the Internal Flow Field for U- and V-shaped Air-Jet Texturing Nozzles
author_sort Jian-Tang Huang
title Compressible Flow Calculations of the Internal Flow Field for U- and V-shaped Air-Jet Texturing Nozzles
title_short Compressible Flow Calculations of the Internal Flow Field for U- and V-shaped Air-Jet Texturing Nozzles
title_full Compressible Flow Calculations of the Internal Flow Field for U- and V-shaped Air-Jet Texturing Nozzles
title_fullStr Compressible Flow Calculations of the Internal Flow Field for U- and V-shaped Air-Jet Texturing Nozzles
title_full_unstemmed Compressible Flow Calculations of the Internal Flow Field for U- and V-shaped Air-Jet Texturing Nozzles
title_sort compressible flow calculations of the internal flow field for u- and v-shaped air-jet texturing nozzles
publishDate 2007
url http://ndltd.ncl.edu.tw/handle/89057676895991652695
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