首页> 外文期刊>Journal of Sound and Vibration >A comparison between off and on-body control surfaces for the FW-H equation: Application to a non-compact landing gear wheel
【24h】

A comparison between off and on-body control surfaces for the FW-H equation: Application to a non-compact landing gear wheel

机译:用于FW-H方程的关闭与体控制表面的比较:应用于非紧凑型起落架

获取原文
获取原文并翻译 | 示例
           

摘要

This work is a contribution to the ongoing debate about the role of quadrupoles in low Mach number flows, studied through the use of solid and permeable surface Ffowcs-Williams & Hawkings (FW-H) integrals for landing gear numerical noise predictions. It rests upon the key idea that the dominance of surface sources over volume sources can only be guaranteed when the compact-source condition is met. We propose here to express this property as a condition on the smallness of the product between the Mach and Strouhal numbers, or formally as MSt < 1. We consider a canonical isolated wheel, that basically consists in a shallow circular cavity inscribed in a coin-like cylinder, thus presenting few different length scales, as compared to a full landing gear assembly. Zonal Detached Eddy Simulations are performed on several gradually refined grids to assess the grid convergence of the numerical result. In particular, important computational effort is put into the accurate resolution of acoustic waves up to Strouhal numbers such that MSt > 1. Overall, determining the real significance of quadrupoles was challenging as numerical errors or misleading effects such as near-field terms, surface discretization, or source domain truncation biased the initial permeable surface results. Even when these sources of bias are removed, non-negligible differences are found between the solid and permeable noise spectra at non-compact St values, while both formulations are equivalent at lower Strouhal numbers. The analysis of these differences is extended to the determination of their impact on frequency-domain noise maps obtained with the DAMAS algorithm fed with far field signals computed with both FW-H approaches. A tentative interpretation of the wheel noise sources is finally proposed, highlighting the dominant role of the scattering of aerodynamic sources by the cavity downstream edge at low Strouhal numbers, while wake sources dominate at higher Strouhal numbers. (C) 2020 Elsevier Ltd. All rights reserved.
机译:这项工作是对正在进行的关于四极在低马赫数流动中的作用的辩论的贡献,通过使用固体和可渗透表面Ffowcs-Williams&Hawkins(FW-H)积分进行起落架数值噪声预测进行研究。它基于这样一个关键思想,即只有在满足紧凑源条件的情况下,才能保证表面源对体积源的主导地位。我们在这里建议将这个性质表示为马赫数和斯特劳哈尔数之间乘积很小的条件,或者形式上表示为MSt<1。我们认为一个典型的孤立车轮,基本上是在一个浅圆腔内刻在类似硬币的圆柱体,因此呈现出不同的长度尺度,相比于一个完整的起落架组件。在几个逐渐细化的网格上进行分区分离涡模拟,以评估数值结果的网格收敛性。特别是,重要的计算工作被投入到声波的精确分辨率,直到斯特鲁哈尔数,使得MSt>1。总的来说,由于数值误差或误导性影响(如近场项、表面离散化或源域截断)使初始可渗透表面结果产生偏差,因此确定四极矩的真正意义具有挑战性。即使消除了这些偏差源,在非紧凑St值下,固体噪声谱和渗透噪声谱之间也存在不可忽略的差异,而在较低的斯特劳哈尔数下,两种公式是等效的。对这些差异的分析扩展到确定它们对DAMAS算法获得的频域噪声图的影响,DAMAS算法由两种FW-H方法计算的远场信号馈送。最后对车轮噪声源进行了初步解释,强调了低斯特鲁哈尔数时空腔下游边缘对空气动力源散射的主导作用,而高斯特鲁哈尔数时尾流源占主导地位。(C) 2020爱思唯尔有限公司版权所有。

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