首页> 外文会议>AIAA/CEAS aeroacoustics conference >Modal Analysis Tools to Enhance FRF-Based Optimization of Vibro-Acoustic Countermeasures in a Turbo-Propeller Aircraft
【24h】

Modal Analysis Tools to Enhance FRF-Based Optimization of Vibro-Acoustic Countermeasures in a Turbo-Propeller Aircraft

机译:模态分析工具,以增强涡轮螺旋桨飞机的振动声对策的基于FRF的优化

获取原文

摘要

This document presents a methodology developed for reducing the total weight of a noise reduction solution with a minimum impact on acoustic performances. This methodology is based on a procedure which identifies, from an optimized solution, the less contributive structural elements to cabin noise. By combining acoustical concepts such as Frequency Response Function (FRF), Modal Participation Factor (MPF) and Modal Acoustic Transfer Vector (MATV), in addition to optimization tools such as Nastran SOL 200, the proposed methodology leads to a significant reduction in weight of the solution with a limited impact on noise reduction values thus obtaining a more effective solution.
机译:本文档介绍了一种用于降低降噪解决方案总重量的方法,并对声学性能的最小影响。该方法基于从优化的解决方案识别的过程,较少的贡献结构元素到舱室噪声。通过组合诸如频率响应功能(FRF)的声学概念,模态参与因子(MPF)和模态声学传递向量(MATV),除了优化工具如NASTRAN SOL 200之外,所述方法还导致重量的显着降低因此,对降噪值的影响有限的溶液因此获得更有效的解决方案。

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