一种计算方法,用于气体填充管中的热声边界层
Nobumasa Sugimoto1, Dai Shimizu2
1Department of Mechanical Engineering, Graduate School of Engineering, University of Osaka, Suita, Osaka 565-0871, Japan.
The Journal of the Acoustical Society of America
|January 4, 2024
概括
本研究介绍了热声边界层的计算方法. 该技术准确计算了边界层边缘的气体速度,这对于热声系统模拟至关重要.
科学领域:
- 物理 物理学 物理
- 流体动力学 流体动力学
- 声学 声学 在声学方面
背景情况:
- 热声系统涉及复杂的边界层现象.
- 对边界层边缘的气体速度进行准确的建模对于模拟至关重要.
- 现有的方法可能缺乏热声边界层分析的精度.
研究的目的:
- 开发和验证用于解决热声边界层方程的计算方法.
- 以数值评估边界层边缘 (vb) 的速度.
- 为热声系统提供数值模拟工具.
主要方法:
- 利用基于使用切比舍夫多项式的序列扩展的计算方法.
- 用可用的分析解决方案解决了一个基准问题.
- 模拟了一个静止的气体,由具有定义声场的脉冲启动.
主要成果:
- 计算方法准确地确定了声场和vb.
- 数字解决方案与分析结果有很好的一致性.
- 该方法在评估边界层速度方面表现出高精度.
结论:
- 开发的计算方法对于热声边界层分析是有效的.
- 这种方法适用于使用边界层理论的数值模拟.
- 精确的vb计算支持热声系统建模的进步.
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