淡江大學機構典藏:Item 987654321/70889
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    Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/70889


    Title: 二維鈍頭體高超音速流場氣體動力分析
    Authors: 歐陽堅;洪祖昌;王政盛
    Contributors: 淡江大學機械與機電工程學系
    Date: 1992-05
    Issue Date: 2011-10-23 21:52:50 (UTC+8)
    Publisher: 臺北市 : 中國航空太空學會
    Abstract: In this paper,Direct Simulation Monte Carlo ( DSMC ) method is used to conduct numerical experiments with the Variable Hard Sphere ( VHS ) molecular model [1] for the low density hypersonic flow . The general flowfield information,Mach number, pressure, density and temperature were obtained for rectangular,round and wedge shaped blunt bodies. The change of flow properties through shock and the effects of rarefaction under different knudsen number can be clearly analyzed by this method.
    Relation: 中國航空太空學會第一屆計算流體力學研討會,頁73-88
    Appears in Collections:[Graduate Institute & Department of Mechanical and Electro-Mechanical Engineering] Proceeding

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