基于波浪-水模型的音爆侵彻CFD研究

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE Transactions of the Japan Society for Aeronautical and Space Sciences Pub Date : 2021-01-01 DOI:10.2322/tjsass.64.273
Po-Hsun Chen, Kojiro Suzuki
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引用次数: 0

摘要

音爆在海洋中的渗透及其影响程度的估计是超声速和高超声速航空的重要课题。大多数先前的研究都是假设浮水表面进行的。然而,众所周知,在真实的海洋环境中,表面波浪度的影响是不可忽略的。本文采用数值方法分析了音爆在空气和水中传播的二维流场。当飞机飞行马赫数高于4.4时,水下流场进入超声速,并在此产生音爆。数值结果表明,在水下亚音速区,穿透波在浮水面和波浪水面下均以消褪波的形式存在,但穿透波是由衰减率较小的波纹引起的。而在超声速水下流动中,水面波浪度对水下音爆侵深几乎没有影响,但会轻微削弱音爆强度。研究了表面波幅对水下穿透波的影响。:
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CFD Study on Penetration of Sonic Boom Applying a Wavy-Water Model
The penetration of sonic booms into the ocean and an estimation of the extent of their in fl uence are important topics for supersonic and hypersonic aviation. Most prior studies were conducted assuming a fl at-water surface. However, it is known that the e ff ect of the surface waviness is not negligible in the case of real ocean environments. In the present study, the numerical method analyzes the two-dimensional fl ow fi eld of sonic boom propagation across the air and water is proposed. When the fl ight Mach number of an aircraft is higher than 4.4, the underwater fl ow fi eld becomes supersonic, and a sonic boom is generated there. The numerical results show that, in the underwater subsonic regime, the penetrating waves have the form of evanescent waves under either fl at or wavy water surface, but the waviness-induced ripples with the smaller decay rate are responsible for deeper penetration. In contrast, in the supersonic underwater fl ow, the surface waviness hardly a ff ects the penetration depth of underwater sonic booms, although it can slightly weaken the boom intensity. The e ff ect of the amplitude of surface waviness on the underwater penetrating wave was also investigated. :
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来源期刊
CiteScore
1.80
自引率
0.00%
发文量
18
审稿时长
>12 weeks
期刊介绍: Information not localized
期刊最新文献
Acknowledgments to Associate Editors Abstracts of the Papers Published in Journal of the Japan Society for Aeronautical and Space Sciences (Vol. 71, No. 6, Dec. 2023) Abstracts of the Papers Published in Journal of the Japan Society for Aeronautical and Space Sciences (Vol. 70, No. 6, Dec. 2022) Analysis of Rotorcraft Vibration Reduction Using a Center-of-Gravity Offset Investigation on Applying an InGaN Photocathode with Negative Electron Affinity for Electric Propulsion
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