在超音速完全发达的流中减轻阻力减轻,并进行间隔吹风
Shibo Lee1, Chenglin Zhou2, Yang Zhang1
1Zhejiang University, Center for Engineering and Scientific Computation and School of Aeronautics and Astronautics, Hangzhou, Zhejiang 310027, People's Republic of China.
Physical review. E
|October 21, 2025
概括
这项关于超音速通道流的研究发现,通过在皮肤摩擦放松阶段定时进行第二次吹风应用来实现最佳的阻力降低. 这种策略增强了旋提升,并减少了剪切应力,以提高性能.
科学领域:
- 流体动力学 流体动力学
- 流建模 流建模
- 超音速流量 超音速流量
背景情况:
- 了解超音速通道流量的阻力减小对于航空航天应用至关重要.
- 与空间发展的流动相比,完全发达的流表现出独特的特征.
- 积极的流量控制方法,如吹风,正在研究空气动力学效率.
研究的目的:
- 为了研究超音速完全发达通道流的阻力和流特性.
- 分析吹风对皮肤摩擦和阻力减轻的影响.
- 确定实施吹风的最佳策略,以最大限度地减少阻力.
主要方法:
- 使用直接数值模拟 (DNS) 来解决流体物理问题.
- 分析皮肤摩擦系数,速度梯度和雷诺兹剪切应力.
- 吹风强度,长度和间隔的参数研究.
主要成果:
- 在完全发达的流中,在吹后观察到皮肤摩擦系数的放松.
- 吹风的强度影响了放松幅度,而不是频率或倾向.
- 通过在放松阶段的初始阻力谷中定时第二次吹风应用来实现最佳阻力减小.
结论:
- 吹风的时间显著影响阻力降低效率.
- 战略吹风应用可以减少速度梯度和雷诺兹剪切应力.
- 通过优化吹风间隔,增强了旋提升和减少了动的皮肤摩擦.
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