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Numerical study of effects of deflected angles of jet fans on the normal ventilation in a curved tunnel

机译:弯道射流扇偏转角对正常通风影响的数值研究

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A computational study was carried out to investigate the effects of deflected angles of jet fans, equipped with silencers, on the tunnel ventilation system. An optimal deflected angle for the normal ventilation in a curved tunnel was proposed. As the fans deflect an angle (β) of 3° towards the convex wall, maximum pressure-rise coefficient and lowest wall shear stress on the ceilings were obtained. An offset of jets on the cross-section was observed for various deflected angles (β) initially. For β = 3°, a relatively gradual velocity profile was obtained as compared to the other values of β which yielded steep velocity profiles downstream. The static pressure increased gradually and overlapped with each other for various values of β initially. The divergence in the longitudinal pressure curves was found when the jets arrived at the curved walls. A relatively shorter distance was required for the pressure-rise to complete at β = 3°.
机译:进行了一项计算研究,研究了装有消音器的喷气风扇的偏转角度对隧道通风系统的影响。提出了弯隧道正常通风的最佳偏转角。当风扇向凸壁偏转3°的角度(β)时,在天花板上可获得最大的压力上升系数和最低的壁切应力。最初,对于各种偏转角(β),观察到横截面上的射流偏移。对于β= 3°,与其他β值相比,获得了一个相对渐进的速度曲线,后者在下游产生了陡峭的速度曲线。最初,静压逐渐增加,并且对于各种β值彼此重叠。当射流到达弯曲的壁时,发现了纵向压力曲线的差异。要使压力上升在β= 3°时需要相对较短的距离。

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