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Aeroelastic simulations of stores in weapon bays using Detached-Eddy simulation

机译:使用Detached-Eddy模拟的武器舱中的商店的气动弹性模拟

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摘要

Detached-Eddy Simulations of flows in weapon bays with a generic store at different positions in the cavity and with flexible fins are presented in this paper. Simulations were carried out to better understand the fluid–structure interactions of the unsteady, turbulent flow and the store. Mach and Reynolds numbers (based on the missile diameter) were 0.85 and 326.000 respectively. Spectral analysis showed few differences in the frequency content in the cavity between the store with rigid and flexible fins. However, a large effect of the store position was seen. When the store was placed inside the cavity, the noise reduction reached 7 dB close to the cavity ceiling. The closer the store to the carriage position, the more coherent and quieter was the cavity. To perform a more realistic simulation, a gap of 0.3% of the store diameter was introduced between the fin root and the body of the store. Store loads showed little differences between the rigid and flexible fins when the store was inside and outside the cavity. With the store at the shear layer, the flexible fins were seen to have a reduction in loads with large fluctuations in position about a mean. Fin-tip displacements of the store inside the cavity were of the range of 0.2% of the store diameter, and in the range of 1–2% of store diameter when at the shear layer.
机译:本文介绍了在武器腔中流动的分离涡流模拟,其中在腔体中的不同位置具有通用存储并且具有柔性鳍片。进行了模拟,以更好地理解非稳态,湍流和储层的流固耦合。马赫数和雷诺数(基于导弹直径)分别为0.85和326.000。频谱分析表明,带有刚性和挠性鳍片的存储之间的腔中频率含量差异很小。但是,看到了存储位置的巨大影响。当将储藏室放置在空腔内时,靠近空腔顶部的噪声降低达到7 dB。商店越接近马车位置,空腔就越连贯且安静。为了执行更逼真的仿真,在鳍根和存储体之间引入了存储直径的0.3%的间隙。当存储在腔体的内部和外部时,存储体的载荷在刚性翅片和柔性翅片之间几乎没有差异。当储存处位于剪切层时,可以看到柔性散热片的负载减少,并且平均位置的波动较大。腔内储层的鳍尖位移在储层直径的0.2%范围内,而在剪切层处则在储层直径的1-2%范围内。

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