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Empirical modelling of noise from high aspect ratio rectangular jets

机译:高长宽比矩形喷口噪声的经验模型

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Noise measurements have been performed on rectangular jets of aspect ratios ranging from 49 to 987 with the aim of determining the appropriate velocity and length scaling to be used in an empirical noise prediction model. The results have shown that the velocity exponent is a function of the nozzle aspect ratio, decreasing with increasing nozzle aspect ratio. In an effort to establish a general prediction model, the velocity exponent of 7 was chosen as the best compromise to represent all the measured data. The analysis of the noise measurements from high aspect ratio nozzles of varying jet height and width has shown that, for the range of aspect ratios considered, the jet sound power level scales with the nozzle height to the power of 3 and the nozzle width to the power of 1. The derived jet noise scaling has been validated with independent experimental data and shows good agreement. (C) 2016 Elsevier Inc. All rights reserved.
机译:已经对纵横比从49到987的矩形射流进行了噪声测量,目的是确定要在经验噪声预测模型中使用的适当速度和长度缩放。结果表明,速度指数是喷嘴长宽比的函数,随着喷嘴长宽比的增加而减小。为了建立通用的预测模型,选择了7的速度指数作为代表所有测量数据的最佳折衷方法。对具有不同喷射高度和宽度的高纵横比喷嘴的噪声测量结果的分析表明,在所考虑的纵横比范围内,喷射声功率级随喷嘴高度缩放为3的幂,而喷嘴宽度变为缩放的比例。 1的幂。导出的射流噪声缩放已通过独立的实验数据进行了验证,并显示出良好的一致性。 (C)2016 Elsevier Inc.保留所有权利。

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