淡江大學機構典藏:Item 987654321/50546
English  |  正體中文  |  简体中文  |  Items with full text/Total items : 62830/95882 (66%)
Visitors : 4049498      Online Users : 843
RC Version 7.0 © Powered By DSPACE, MIT. Enhanced by NTU Library & TKU Library IR team.
Scope Tips:
  • please add "double quotation mark" for query phrases to get precise results
  • please goto advance search for comprehansive author search
  • Adv. Search
    HomeLoginUploadHelpAboutAdminister Goto mobile version
    Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/50546


    Title: Reduced Navier-Stokes Simulation of Incompressible Microchannel Flows
    Authors: Chen, Ching Shung
    Contributors: 淡江大學航空太空工程學系
    Keywords: Computer simulation;Friction;Incompressible flow;Navier Stokes equations;Thermal conductivity;Viscosity;Incompressible microchannel flows;Microchannels
    Date: 2008-01
    Issue Date: 2013-03-20 16:27:23 (UTC+8)
    Publisher: Philadelphia: Taylor & Francis Inc.
    Abstract: The objective of this research is to investigate numerically the effects of temperature dependent viscosity and thermal conductivity on friction characteristics of incompressible flow in long microchannels involving large temperature variations. The physical properties of water change significantly with temperature. These property changes result in highly nonlinear temperature, pressure, Reynolds number, and f Re distributions along the microchannel axis. These temperature effects must be taken into account to accurately predict the friction characteristics of incompressible microchannel flows. The major advantage of the present numerical procedure is its fast speed due to the parabolic character of the governing equations and the finite-difference method used. It is at least two to three orders of magnitude faster than the full Navier-Stokes simulation.
    Relation: Numerical Heat Transfer, Part A: Applications 53(1), pp.71-87
    DOI: 10.1080/10407780701453727
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Journal Article

    Files in This Item:

    File SizeFormat
    index.html0KbHTML288View/Open

    All items in 機構典藏 are protected by copyright, with all rights reserved.


    DSpace Software Copyright © 2002-2004  MIT &  Hewlett-Packard  /   Enhanced by   NTU Library & TKU Library IR teams. Copyright ©   - Feedback