Numerical Simulations of Gaseous Slip Flow in Micro-channels

碩士 === 淡江大學 === 航空太空工程學系 === 87 === The objective of present work is to investigate gaseous flow in micro-channels analytically as well as numerically and compare the results with experiment data. Gaseous flow is typically classified into one of four flow regions according to its Knudsen...

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Main Authors: Fu-Chih Yu, 余福治
Other Authors: Ching-Shung Chen
Format: Others
Language:zh-TW
Published: 1998
Online Access:http://ndltd.ncl.edu.tw/handle/34524599447675280574
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spelling ndltd-TW-087TKU002950052016-02-01T04:13:05Z http://ndltd.ncl.edu.tw/handle/34524599447675280574 Numerical Simulations of Gaseous Slip Flow in Micro-channels 可滑動氣流在長微流道內之數值分析 Fu-Chih Yu 余福治 碩士 淡江大學 航空太空工程學系 87 The objective of present work is to investigate gaseous flow in micro-channels analytically as well as numerically and compare the results with experiment data. Gaseous flow is typically classified into one of four flow regions according to its Knudsen number. These regions are continuum flow, slip flow, transition flow, and free molecular flow. The proposed model assumes the flow is a continuum but employs a slip condition on the channel wall. Although numerical methods for solving the compressible Navior-Stokes equations can be used to study this problem, they are inefficient due to their hyperbolic-parabolic character. The results of present work show that slip flow can be predicted accurately by solving the compressible boundary-layer equations. The parabolic character of the boundary-layer equations renders the present method a very efficient and accurate tool in studying slip flow. The results of present work reveal some interesting features of slip micro-channel flows. First, due to the extraordinarily small dimensions, a large pressure gradient is required to drive the flow. Although the pressure gradient is large, the velocity remains very small due to the high shear stress on the wall, and the corresponding Reynolds number is also relatively small, so that the flow can be safely assumed to be laminar. Second, diffusion is the dominant momentum and energy transfer mechanism in micro-channel. The results also show that the slip boundary condition, which is the result of incomplete momentum and energy exchanges between the impinging gas molecules and the walls, has decisive effects on velocity and therefore mass flow rate of the flow. The computed results are compared with experimental data and theoretical solution. The agreement is quite good. It indicates that the slip model of this study is indeed able to predict micro-channel flows in the slip region, but further study is needed for flows in the transition or free molecular regions. Ching-Shung Chen 陳慶祥 1998 學位論文 ; thesis 81 zh-TW
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description 碩士 === 淡江大學 === 航空太空工程學系 === 87 === The objective of present work is to investigate gaseous flow in micro-channels analytically as well as numerically and compare the results with experiment data. Gaseous flow is typically classified into one of four flow regions according to its Knudsen number. These regions are continuum flow, slip flow, transition flow, and free molecular flow. The proposed model assumes the flow is a continuum but employs a slip condition on the channel wall. Although numerical methods for solving the compressible Navior-Stokes equations can be used to study this problem, they are inefficient due to their hyperbolic-parabolic character. The results of present work show that slip flow can be predicted accurately by solving the compressible boundary-layer equations. The parabolic character of the boundary-layer equations renders the present method a very efficient and accurate tool in studying slip flow. The results of present work reveal some interesting features of slip micro-channel flows. First, due to the extraordinarily small dimensions, a large pressure gradient is required to drive the flow. Although the pressure gradient is large, the velocity remains very small due to the high shear stress on the wall, and the corresponding Reynolds number is also relatively small, so that the flow can be safely assumed to be laminar. Second, diffusion is the dominant momentum and energy transfer mechanism in micro-channel. The results also show that the slip boundary condition, which is the result of incomplete momentum and energy exchanges between the impinging gas molecules and the walls, has decisive effects on velocity and therefore mass flow rate of the flow. The computed results are compared with experimental data and theoretical solution. The agreement is quite good. It indicates that the slip model of this study is indeed able to predict micro-channel flows in the slip region, but further study is needed for flows in the transition or free molecular regions.
author2 Ching-Shung Chen
author_facet Ching-Shung Chen
Fu-Chih Yu
余福治
author Fu-Chih Yu
余福治
spellingShingle Fu-Chih Yu
余福治
Numerical Simulations of Gaseous Slip Flow in Micro-channels
author_sort Fu-Chih Yu
title Numerical Simulations of Gaseous Slip Flow in Micro-channels
title_short Numerical Simulations of Gaseous Slip Flow in Micro-channels
title_full Numerical Simulations of Gaseous Slip Flow in Micro-channels
title_fullStr Numerical Simulations of Gaseous Slip Flow in Micro-channels
title_full_unstemmed Numerical Simulations of Gaseous Slip Flow in Micro-channels
title_sort numerical simulations of gaseous slip flow in micro-channels
publishDate 1998
url http://ndltd.ncl.edu.tw/handle/34524599447675280574
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