淡江大學機構典藏:Item 987654321/109038
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    题名: Numerical Investigations of Body Tail Projectile
    作者: Elnaggar, Wessam Mahfouz;Chen, Zhi-Hua;Huang, Zhen-Gui
    关键词: Body Tail Projectile;Aerodynamic Coefficients;FLUENT
    日期: 2016-06
    上传时间: 2016-12-27 09:40:40 (UTC+8)
    摘要: The unsteady compressible flow around a body tail projectile is numerically solved with a
    Large Eddy Simulation (LES) method, Smagorinsky-Lilly model was used as the Sub-Grid Scale (SGS). The computed results are obtained in supersonic flow regime for a viscous fluid in order to
    determine the aerodynamic coefficients with different angles of attack. The flow around a body tail projectile was solved as a three-dimensional flow.
    關聯: Journal of Applied Science and Engineering 19(2),pp. 163-168
    DOI: 10.6180/jase.2016.19.2.06
    显示于类别:[淡江理工學刊] 第19卷第2期

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