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    Please use this identifier to cite or link to this item: http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/38451

    Title: 穿音速三維流場之數值模擬
    Other Titles: Numerical simulation of transonic inviscid flow about three-dimensional configurations
    Authors: 宛同;Wan, Tung;范代禧;Fan, Tai-Hsi
    Contributors: 淡江大學航空太空工程學系
    Keywords: 穿音速流;數值模擬;可調適格點;翼體;馬赫數;攻角;Transonic Flow;Numerical Simulation;Adaptive Grid;Wing-Body;Mach Number;Angle Of Attack
    Date: 1992-05
    Issue Date: 2010-01-11 15:17:52 (UTC+8)
    Abstract: A fast, conservative finite difference scheme for the full potential equation has been applied to the three- dimensional transonic flows. This scheme employes the standard approximate factorization ( AF2), upwind bias, temporal damping, and a specific .alpha.-sequence acceleration techniques. To achieve faster and more accurate results, an adaptive grid method using the tension and torsion spring analogies is also being developed. The resulting flow field calculations of half-span, full-span wing, and wing-body combination with different Mach numbers, angles of attack, and sideslip angles show the feasibility and validity of the current method.
    Relation: 中國航空太空學會第一屆計算流體力學研討會論文集=Proceedings of the First National Conference on Computational Fluid Dyna mics,頁133-141
    Appears in Collections:[Graduate Institute & Department of Aerospace Engineering] Proceeding

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