淡江大學機構典藏:Item 987654321/38271
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    Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/38271


    Title: Flux-spline method for compressible navier-stokes flow at low mach number
    Other Titles: 以 flux-spline 方法解析低馬赫數的黏性壓縮層流
    Authors: Sheu, Tony W. H.;Lin, C. Y.;Lee, S. M.
    Contributors: 淡江大學航空太空工程學系
    Date: 1989-12
    Issue Date: 2010-01-11 15:00:20 (UTC+8)
    Publisher: 成功大學
    Abstract: 以SMAC 有限差分方法探討浮懸在水域上油滴顆粒的傳送現象。主要變數如速度和壓力的數值是
    由SOR 求得。計算的結果和由SI MPLER的解作比較。油滴和水粒子之間的作用力在本分析中
    不于考慮。油滴的傳送現象由其位置的改變表示。
    A flux-spline scheme for total flux terms is developed for increasing accuracy
    in7yhace. The resulting discretized equations are solved using ICE algorithm such
    that larger stability limit is allowed for solving low Mach number flowfield. The
    evaluation of transient driven cavity flowfield is analyzed and good agreement with
    SOLA-ICE is obtained.
    Relation: 中國機械工程學會第六屆學術研討會論文集(一), pp.215-222
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Proceeding

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