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    Please use this identifier to cite or link to this item: http://chur.chu.edu.tw/handle/987654321/35023


    Title: A ROBUST AND SIMPLE LOW-MACH NUMBER SOLVER FOR FLAPPING-WING SIMULATIONS
    Authors: 牛仰堯
    Niu, Yang-Yao
    Contributors: 機械工程學系
    Mechanical Engineering
    Keywords: Navier–Stokes equations;unsteady preconditioned compressible flow code;biological aerodynamics;flapping wing;propulsive efficiency
    Date: 2011
    Issue Date: 2014-06-27 03:17:49 (UTC+8)
    Abstract: In the current study, a very simple preconditioned Navier-Stokes solver based on Roe type numerical fluxes is developed to investigate the unsteady aerodynamics around the flapping wings. A modified Osher-Chakravarthy (MOC) upwind finite-volume scheme is
    Appears in Collections:[Department of Mechanical Engineering] Seminar papers

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