基于声学模式的直升机噪声足迹的全球预测和分析
Mengxue Shao1, Yang Lu1, Xice Xu1
1National Key Laboratory of Helicopter Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China.
The Journal of the Acoustical Society of America
|September 18, 2024
概括
一个新的声学模态过程可以有效地预测直升机转子噪声足迹. 这种方法显著减少了噪声评估的计算时间,有利于航空应用.
科学领域:
- 声学 声学 在声学上.
- 航空航天工程 航空航天工程
- 计算流体动力学的流体动力学.
背景情况:
- 直升机旋转器噪声带来了重大的环境挑战.
- 准确预测噪声足迹对于运营规划和公众接受至关重要.
- 现有的方法可能是计算密集型,限制实时应用.
研究的目的:
- 开发一个集成的,计算效率高的流程,用于预测直升机旋转机的全球噪声足迹.
- 为了利用声学模式进行更快,更全面的噪音分析.
- 评估飞行参数 (如下降角度和前进比) 对噪声辐射的影响.
主要方法:
- 通过将时间域的声压映射到模态系数来构建一个声学模态数据库.
- 编目各种飞行状态的声学模式系数.
- 基于轨迹参数的提取系数用于噪声足迹评估.
- 使用AS350直升机模型进行模拟研究.
主要成果:
- 开发的声学模态过程提供了全球预测和分析能力.
- 这种方法可以显著减少计算时间,大约是传统方法的五分之一.
- 该研究模拟了AS350直升机在前进和接近飞行阶段的噪音影响.
- 对于一个拥有1800名观察员的区域,观察到计算时间的减少.
结论:
- 综合声学模态过程为直升机噪声足迹评估提供了高效和实用的解决方案.
- 该方法的低计算成本和全球预测能力提高了其在军事和民用航空中的实用性.
- 这种方法为旋翼飞机运营提供了更有效的噪音管理策略.
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