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马赫数在低音共流喷气中因唇厚变化而发生的特征变化
K Sathish Kumar1, R Naren Shankar2, V G Ganesan3
1Department of Aeronautical Engineering, Nehru Institute of Engineering and Technology, T.M Palayam, Coimbatore, Tamil Nadu, India.
Scientific reports
|November 26, 2025
概括
在共流喷气中变化的唇厚显著减少了潜在的核心长度,增强了喷气混合以减少噪音. 更高的绕道比率进一步降低了潜在的核心长度,特别是在更厚的嘴唇上.
科学领域:
- 航空航天工程 航空航天工程
- 流体动力学 流体动力学
- 声学 声学 在声学方面
背景情况:
- 减少喷气式飞机噪音对于飞机效率和环境影响至关重要.
- 被动流量控制方法,如变化唇厚,为喷射混合增强提供了潜力.
- 了解潜在的核心长度减小是改善喷气混合的关键.
研究的目的:
- 为了研究低音共流喷气机马赫数衰变的新型属性.
- 分析不同唇厚和绕道比对潜在核心长度的影响.
- 探索用于喷气混合增强的被动控制策略.
主要方法:
- 实验研究低音共流喷气的马赫数为0.6.6.
- 使用了三种唇厚 (2毫米,10毫米,15毫米) 和从0.7到6.4.4的绕道比率.
- 采用Pitot静态测量和验证的数值模拟来进行流量分析.
主要成果:
- 一个10毫米的嘴唇厚度将潜在的核心长度降低了高达45% (在绕道比率为6.4).
- 一个15毫米的嘴唇厚度将潜在的核心长度降低了高达58% (在绕道比率6时).
- 增加的绕道比率始终降低了更厚的嘴唇的潜在核心长度.
结论:
- 厚唇共同流动的喷流显示了再循环区域和初始中线马赫数的增加.
- 嘴唇厚度和绕道比是减少潜在核心长度的有效参数.
- 这些发现支持被动控制策略,以提高喷气混合和降低噪音.
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