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    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/109038

    Title: Numerical Investigations of Body Tail Projectile
    Authors: Elnaggar, Wessam Mahfouz;Chen, Zhi-Hua;Huang, Zhen-Gui
    Keywords: Body Tail Projectile;Aerodynamic Coefficients;FLUENT
    Date: 2016-06
    Issue Date: 2016-12-27 09:40:40 (UTC+8)
    Abstract: 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.
    Relation: Journal of Applied Science and Engineering 19(2),pp. 163-168
    DOI: 10.6180/jase.2016.19.2.06
    Appears in Collections:[Journal of Applied Science and Engineering] v.19 n.1

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