在小型无人机中对转子束配置的航空声学调查
Jose Rendón-Arredondo1, Emma Vella1,2, Andrea Arroyo Ramo1
1Université de Sherbrooke, Sherbrooke, Québec J1K2R1, Canada.
The Journal of the Acoustical Society of America
|August 14, 2025
概括
这项研究调查了无人机中的转子束空气声学,发现不稳定的加载噪声占主导地位. 数字和分析模型准确地预测了噪音,揭示了小型无人机独特的声音模式.
科学领域:
- 声学 声学 声学 声学
- 空气动力学 在空气动力学.
- 计算流体动力学的流体动力学.
背景情况:
- 转子束配置在小型无人机中很常见.
- 了解它们的空气声学机制对于降低噪声至关重要.
研究的目的:
- 为了研究小型无人机的转子束配置中的空气声学机制.
- 开发和验证用于预测转子束噪声的数值和分析模型.
主要方法:
- 高保真格子-博尔兹曼方法 (LBM) 模拟.
- 威廉姆斯和霍金斯 (FW-H) 的声学类比.
- 使用条形理论和西尔斯叶片响应函数的频域分析模型.
主要成果:
- 腰部瘤模拟和分析模型与实验数据有很好的一致性.
- 不稳定的加载噪声被确定为所有音调的主导噪声源.
- 在声音波的三维方向性中观察到独特的波形图案.
结论:
- 开发的模型准确地预测了转子束噪声.
- 不稳定的加载噪声对于小型无人机噪声管理至关重要.
- 对观察到的声音和模式进行进一步的研究是有必要的.
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