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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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 |
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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.
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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 |
work_keys_str_mv |
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