首页> 外文会议>ASME Fluids Engineering Division summer conference;FEDSM2008 >NUMERICAL EFFECT OF AIRFLOW FROM A LOWER CANOPY (BLUFF BODY) INTO AN UPPER CANOPY IN STEADY AND TURBULENT CONDITION
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NUMERICAL EFFECT OF AIRFLOW FROM A LOWER CANOPY (BLUFF BODY) INTO AN UPPER CANOPY IN STEADY AND TURBULENT CONDITION

机译:在稳态和湍流条件下,下冠层(风琴体)到上冠层的气流的数值效果

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In this paper, a 3-D flow field around two bluff bodies in an incompressible fluid is modeled [1]. Formations of these two bodies are top to top (One on the top of the other) with respect to the center of each other. The lower on has a constant cross sectional area with a vent of air at its apex and the upper one has a variable cross sectional area with no vent on it.The vertical distances between the bluff bodies, the cross sectional area, and also the vent ratio of bluff bodies are varied here. Vertical distances of these two bodies are varied form zero to half, equal, double and triple the radius of the body with a vent on it (lower body). Flow condition is considered 3D, steady, turbulent, and incompressible. The drag force on each body and also the pressure around the two bodies are calculated. From the numerical results, it can be seen that, the drag force is constant over the range of zero to twenty percent of the vent ratios and for higher vent ratios when the upper bluff body is smaller than the lower one the drag force decreased, and it increased when the upper bluff body is larger than the lower one.
机译:在本文中,对不可压缩流体中两个钝体周围的3-D流场进行了建模[1]。相对于彼此的中心,这两个物体的形成是自上而下的(一个在另一个的顶部)。下部具有恒定的横截面积,在其顶部具有排气孔,而上部具有可变的横截面积,其上没有排气孔。 在此改变阻流体的垂直距离,横截面积以及阻流体的通风比。这两个物体的垂直距离的变化范围为具有排气孔(下部物体)的物体半径的0到一半,相等,两倍和三倍。流动条件被认为是3D,稳定,湍流和不可压缩的。计算每个物体上的阻力以及两个物体周围的压力。从数值结果可以看出,阻力在通气比的百分之零到百分之二十的范围内是恒定的;对于较高的通气比,当上阻流体小于下阻流体时,阻力减小,并且当上部的虚张声势体大于下部的虚张声势体时,它会增加。

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