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含激波的湍流流动高精度大涡数值模拟方法(英文) 被引量:1
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作者 D.V.Kotov H.C.Yee +2 位作者 A.Wray a.hadjadj B.Sjogreen 《空气动力学学报》 CSCD 北大核心 2016年第2期190-203,共14页
针对采用亚格子模型进行含激波的湍流流动模拟时会面临激波附近的精度损失问题,考虑从通过亚格子模型以及数值模拟方法两方面的改进来实现湍流流动大涡模拟的精度提高。大涡模拟采用了Yee及Sjgreen(2009)提出的高阶低耗散方法。该方... 针对采用亚格子模型进行含激波的湍流流动模拟时会面临激波附近的精度损失问题,考虑从通过亚格子模型以及数值模拟方法两方面的改进来实现湍流流动大涡模拟的精度提高。大涡模拟采用了Yee及Sjgreen(2009)提出的高阶低耗散方法。该方法采用自适应的流场探测器以控制计算中所需区域的数值耗散,并考虑对动力学模型采用在激波位置使用Sagaut和Germano(2005)提出的单边亚格子过滤器和(或)直接禁用亚格子项等方法加以改进。对于标准的马赫数1.5和3条件下的激波-湍流干扰问题,上述新方法相较于全区域采用亚格子模型的方法均表现出了相似的精度提升。同时实现的数值精度改进方案采用了Harten的亚单元分辨过程来定位和锐化激波,并在精确激波位置附近的网格点处采用了单边测试滤波。 展开更多
关键词 高阶低耗散格式 Germao模型 大涡模拟滤波 直接数值模拟方法 亚单元分辨格式 激波湍流干扰
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Achieving an optimal shock-wave mitigation inside open channels with cavities for weak shock waves:A computational study
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作者 N.Brahmi a.hadjadj 《Theoretical & Applied Mechanics Letters》 CAS CSCD 2020年第5期354-365,共12页
This paper deals with a numerical study of weak shock-waves propagation and their attenuation in channel flow having different heights and exhibiting a hollow circular cavities with different depths and diffraction an... This paper deals with a numerical study of weak shock-waves propagation and their attenuation in channel flow having different heights and exhibiting a hollow circular cavities with different depths and diffraction angles inside.The effect of initial diffraction angle and cavity depth on the shock mitigation is investigated.A better shock attenuation is achieved with diffraction angle by a factor of approximately 17%in terms of shock-Mach number and 38%in terms of total energy.The obtained results show also,in addition to the initial diffraction angle and cavity depth,the importance of reducing the channel heights as well as the position of the reduced section in achieving an optimal shock-wave attenuation.The presence of a cavity inside the channel helps to attenuate faster the shock wave.The underlying physics relies on the shock diffraction phenomenon that generates large amount of vortical structures capable of dissipating part of the shock energy by inducing a pressure loss behind it.A subtle arrangement of channel position/height and a cavity location leads to an efficient pressure attenuation by approximately a factor of 57%forMs=1.6 and 16%for Ms=1.1.. 展开更多
关键词 Shock diffraction Shock reflection Shock attenuation Vortex generation
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