Analysis of fluid flow through micro-fluidic devices using characteristic-based-split procedure

Gas flow in micro‐electro‐mechanical systems can be considered as rarefied since the ratio of free molecular path length to the characteristic length of the device is high. It is possible to analyse these flows using a conventional Navier–Stokes solver with modified boundary conditions to account fo...

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Bibliographic Details
Published inInternational journal for numerical methods in fluids Vol. 51; no. 9-10; pp. 1041 - 1057
Main Authors Celik, Bayram, Edis, Firat Oguz
Format Journal Article Conference Proceeding
LanguageEnglish
Published Chichester, UK John Wiley & Sons, Ltd 30.07.2006
Wiley
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ISSN0271-2091
1097-0363
1097-0363
DOI10.1002/fld.1197

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Summary:Gas flow in micro‐electro‐mechanical systems can be considered as rarefied since the ratio of free molecular path length to the characteristic length of the device is high. It is possible to analyse these flows using a conventional Navier–Stokes solver with modified boundary conditions to account for temperature‐jump and slip‐velocity on solid walls. In this study, characteristic‐based‐split (CBS) algorithm is modified to account for slip‐velocity and temperature‐jump boundary conditions in order to perform compressible flow analysis for a micro sized geometry. The CBS algorithm is a split procedure which yields a unified solution method valid for both compressible and incompressible flows. To verify the modified CBS solver, straight micro channel and micro step duct geometries are selected as test cases. To reduce the size of the implicit part of the algorithm, pseudo‐quadratic velocity/linear pressure elements (pP2P1) are employed. The results obtained using CBS algorithm, are compared with other analytical and computational results available in the literature. It is shown that this implementation of the CBS algorithm is applicable and effective for micro gas flows. It is also shown that, increasing Knudsen number results in increased temperature‐jump and slip‐velocity. This effect, however, is limited, especially for high Mach number flows. Copyright © 2006 John Wiley & Sons, Ltd.
Bibliography:istex:148BC37708C739904D9DA2C047E0BDE4707AAD9D
Istanbul Technical University - No. 1839
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ArticleID:FLD1197
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ISSN:0271-2091
1097-0363
1097-0363
DOI:10.1002/fld.1197