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Periodic acoustic radiation from a low aspect ratio propeller.

机译:低纵横比螺旋桨发出的周期性声辐射。

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摘要

An experimental program was conducted with the objective of providing high fidelity measurements of propeller inflow, unsteady blade surface pressures, and discrete acoustic radiation over a wide range of speeds. Anechoic wind tunnel experiments were preformed using the SISUP propeller. The upstream stator blades generate large wake deficits that result in periodic unsteady blade forces that acoustically radiate at blade passing frequency and higher harmonics. The experimental portion of this research successfully measured the inflow velocity, blade span unsteady pressures and directive characteristics of the blade-rate radiated noise associated with this complex propeller geometry while the propeller was operating on design.; The spatial harmonic decomposition of the inflow revealed significant coefficients at 8, 16 and 24. The magnitude of the unsteady blade forces scale as U4 and linearly shift in frequency with speed. The magnitude of the discrete frequency acoustic levels associated with blade rate scale as U6 and also shift linearly with speed. At blade-rate, the far-field acoustic directivity has a dipole-like directivity oriented perpendicular to the inflow. At the first harmonic of blade-rate, the far-field directivity is not as well defined.; The experimental inflow and blade surface pressure results were used to generate an acoustic prediction at blade rate based on a blade strip theory model developed by Blake (1986). The predicted acoustic levels were compared to the experimental results.; The model adequately predicts the measured sound field at blade rate at 120 ft/sec. Radiated noise at blade-rate for 120 ft/s can be described by a dipole, whose orientation is perpendicular to the flow and is generated by the interaction of the rotating propeller with the 8th harmonic of the inflow. At blade-rate for 60 ft/s, the model under predicts measured levels.; At the first harmonic of blade-rate, for 120 ft/s, the sound field is described as a combination of dipole sources, one generated by the 16 th harmonic, perpendicular to the inflow, and the other generated by the 12th harmonic of the inflow parallel to the inflow. At the first harmonic of blade-rate for 60 ft/s, the model under predicts measured levels.
机译:进行了一个实验程序,目的是在很大的速度范围内提供高保真度的螺旋桨流入量,不稳定的叶片表面压力以及离散的声辐射。使用SISUP螺旋桨进行了消声风洞实验。上游的定子叶片会产生较大的尾流缺陷,从而导致周期性的非稳态叶片力以叶片通过频率和更高的谐波声辐射。该研究的实验部分成功地测量了螺旋桨在设计过程中与这种复杂螺旋桨几何形状相关的流入速度,叶片跨度非定常压力以及叶片速率辐射噪声的定向特性。流入的空间谐波分解在8、16和24处显示出显着的系数。不稳定叶片力的大小按 U 4 缩放,并且频率随速度线性变化。与叶片速率标度相关的离散频率声级的大小为 U 6 ,并且随速度线性变化。在叶片速率下,远场声指向性具有垂直于流入方向定向的偶极状指向性。在叶片速度的一次谐波处,远场方向性没有很好地定义。基于Blake(1986)开发的叶片条理论模型,将实验的入流量和叶片表面压力结果用于以叶片速率生成声学预测。将预测的声级与实验结果进行比较。该模型可以以120英尺/秒的叶片速率充分预测测得的声场。叶片速率为120 ft / s时的辐射噪声可以用偶极子描述,该偶极子的方向垂直于流,并且是由旋转螺旋桨与流入的第8次谐波相互作用产生的。 。在叶片速率为60 ft / s的情况下,该模型将预测测得的水平。在叶片速率的一次谐波下,对于120 ft / s,声场被描述为偶极子源的组合,一个偶极子源是由16 谐波产生的,垂直于流入,而另一个由平行于入流的第十二个 谐波产生的。在叶片速率为60 ft / s的第一次谐波时,该模型将预测测得的水平。

著录项

  • 作者

    Muench, John David.;

  • 作者单位

    University of Rhode Island.;

  • 授予单位 University of Rhode Island.;
  • 学科 Engineering Mechanical.; Physics Acoustics.
  • 学位 Ph.D.
  • 年度 2001
  • 页码 291 p.
  • 总页数 291
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;声学;
  • 关键词

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