首页> 外文会议>AIAA/CEAS aeroacoustics conference >Noise prediction for serrated leading-edges
【24h】

Noise prediction for serrated leading-edges

机译:锯齿状引导边缘的噪声预测

获取原文

摘要

Amiet's theory offers an efficient and accurate means of predicting trailing edge and leading edge noise, but it assumes that the edge is straight and cannot be applied to serrated edges. Serrations are known to be effective at reducing trailing edge and leading edge noise, but little theoretical work has been carried out on predicting the amount of noise reduction. A recently developed model that generalises Amiet's theory for trailing edge noise with sawtooth trailing edges predicts noise reduction levels of 5-10 dB that are close to experimental measurements. Such generalised Amiet's theory has yet to be developed for serrated leading edges. There is currently no analytical model that is applicable to serrated leading edges, and such model could play a key role in the design of quieter turbofan engines. This paper derives a generalised Amiet model for predicting leading edge noise with a sawtooth leading edge and validates the noise prediction against experimental results. This work will shed light into the noise reduction mechanism due to serrated leading edges and will help design more effective serrations.
机译:Amiet的理论提供了一种高效且准确的方法,可以预测后缘和前缘噪音,但它假设边缘是直的并且不能应用于锯齿状边缘。已知锯齿可有效地减少后缘和前沿噪声,但是在预测降噪量的情况下已经进行了很少的理论工作。最近开发的模型,揭开亚丽培的尾部噪声理论,锯齿尾部边缘预测近于实验测量的5-10 dB的降噪水平。这种广义的亚派的理论尚未开发出锯齿状的领先边缘。目前没有适用于锯齿状的领先边缘的分析模型,此类模型可以在更安静的涡扇发动机设计中发挥关键作用。本文推出了一种推广的亚煤层模型,用于预测具有锯齿前沿的前缘噪声,并验证对实验结果的噪声预测。由于锯齿状的领先边缘,这项工作将闪光进入降噪机制,并有助于设计更有效的锯齿。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号