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    Please use this identifier to cite or link to this item: http://chur.chu.edu.tw/handle/987654321/34061


    Title: 超音速噴流數值研究
    Authors: 蔡永培
    Tsai, Yeong-Pei
    Contributors: 機械工程學系
    Mechanical Engineering
    Keywords: 關鍵字;噴射流;超音速;加權型基本不震盪算則
    Keywords;Jet;Supersonic;WENO
    Date: 2008
    Issue Date: 2014-06-27 02:38:24 (UTC+8)
    Abstract: 本論文之研究為建立一分析超音速可壓縮流之
    噴流流場。在數值方法的選擇上,採取可壓縮流領域
    中的加權型基本不震盪算則直接求解Navier-Stokes
    方程式。而程式撰寫技巧上採用具增強數值穩定性的
    Lower-upper Symmetric successive over
    relaxation ( LU-SSOR method ) 以增強數值之穩定
    性及加速程式之收斂。文中包含了平板噴流的渦漩運
    動的特性及紊流超音速混合層的特性,其結果顯示都
    有不錯的精確度。
    The basic idea of this research is to establish a
    numerical simulation,which analyzes the effect of
    compressibility of supersonic jet flow phenomena. The
    numerical simulation method adopted is the "WENO"
    schem developed for compressible flow solving the
    N
    Appears in Collections:[Department of Mechanical Engineering] Seminar papers

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