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罗西特方程:改善分数旋速度,并定义空洞流动的有效长度与深度比
Matthew Gabel1, Nesrin Sarigul-Klijn1
1DynaaTECC Research Lab, Mechanical and Aerospace Engineering, University of California, Davis, Davis, California 95616-5294, USA.
The Journal of the Acoustical Society of America
|February 11, 2024
概括
这项研究通过结合分析技术和引入有效的长度与深度比率方法来增强可压缩流中的空腔模式预测. 分数旋速度是通过马赫数来计算未来预测的.
科学领域:
- 流体动力学 流体动力学
- 声学 声学 在声学方面
- 空气动力学 航空动力学
背景情况:
- 罗西特模式对于理解可压缩流中的腔体声学至关重要.
- 现有的分析技术需要改进才能准确预测.
- 腔共振现象是复杂的,并且根据流量条件而有所变化.
研究的目的:
- 审查和结合现有的分析方法来预测可压缩流中的Rossiter模式.
- 引入一种新的实验方法来预测空洞频率,使用有效的长度与深度比.
- 为增强的预测模型,在广泛的马赫数范围内计算分数旋速度.
主要方法:
- 审查和整合已建立的分析技术用于Rossiter模式预测.
- 开发一种新方法,利用从实验数据中得出的洞穴有效长度与深度比.
- 从高次声速 (马赫0.55) 到超声速 (马赫2.3) 的分数旋速度的计算.
主要成果:
- 对于可压缩流量条件的组合分析方法的性能提高.
- 一种经过验证的方法,用于预测各种马赫数的腔共振频率.
- 对于未来的空气动力学声学应用,关于分数旋速度的全面数据.
结论:
- 综合分析和实验方法为Rossiter模式预测提供了更高的准确性.
- 有效的长度与深度比为频率预测提供了有价值的参数.
- 计算的分数旋速度对于推进腔体声学研究至关重要.
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