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Perforated ventilation ducts: Part 2, validation of an air distribution model.

机译:多孔通风管:第2部分,空气分配模型的验证。

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The mathematical model for air flow distribution pattern in a perforated duct was validated by measuring the flow performance in 4 experimental ducts with aperture ratios of 0.5, 1.0, 1.5 and 2.0. The basic assumptions of the model were upheld. Theskin friction loss calculated from the momentum equation was the same as that provided by the energy equation. The energy equation can be used to evaluate the regain coefficient without considering friction losses. The regain coefficient and the energy correction factor were almost unity for turbulent flow. The discharge coefficient was constant and approximately 0.65, along the full length of the perforated duct. Frictional losses occurred along the length of the duct but had no significant effect on the discharge angle. The discharge angle (alpha) can be calculated from the duct average air velocity (V) and the potential outlet air jet velocity (V0).
机译:通过测量孔径比为0.5、1.0、1.5和2.0的4个实验导管的流动性能,验证了多孔导管中气流分布模式的数学模型。该模型的基本假设得以维持。由动量方程式计算的皮肤摩擦损失与能量方程式所提供的相同。能量方程式可用于评估回潮系数,而无需考虑摩擦损耗。回流系数和能量校正因子对于湍流几乎是统一的。沿穿孔管的整个长度方向,排出系数恒定且约为0.65。摩擦损失沿导管的长度方向发生,但对排出角度没有明显影响。可以从管道平均空气速度(V)和潜在的出口空气喷射速度(V0)计算出排放角(α)。

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