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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering >Numerical study on self-sustained oscillation characteristics of cavity flameholders in a supersonic flow
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Numerical study on self-sustained oscillation characteristics of cavity flameholders in a supersonic flow

机译:超声速流中腔型火焰保持器自持振荡特性的数值研究

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Self-sustained oscillation characteristics of two-dimensional cavity-based flameholders in a cold supersonic flow were investigated in the present numerical study. The unsteady flowfields were calculated using hybrid Reynolds-averaged Navier–Stokes/large eddy simulation (RANS/LES) method. The key cavity parameters that were varied include cavity aft wall angle and cavity length to depth ratio. The hybrid model favourably captured the large scale unsteady characteristics and revealed the evolution process of cavity free shear layer. Pressure fluctuation spectra agreed well with theoretical predictions. The hybrid RANS/LES data indicate that cavity shape and size both have significant effects on the oscillation characteristics. As the cavity length to depth ratio decreases, oscillation frequency corresponding to maximum oscillation amplitude shifts to higher values. Most of the oscillation modes are greatly suppressed as the cavity aft wall angle decreases. Contrast to the steep aft wall cavity, only higher frequency modes remain in the oscillation of the cavity with small aft wall angle.
机译:在本数值研究中,研究了二维腔型火焰保持器在超音速冷流中的自持振荡特性。使用混合雷诺平均Navier-Stokes /大涡模拟(RANS / LES)方法计算非稳态流场。改变的关键腔参数包括腔后壁角度和腔长深比。混合模型很好地捕捉了大规模的非稳态特征,揭示了无腔剪切层的演化过程。压力波动谱与理论预测吻合良好。混合的RANS / LES数据表明,腔体的形状和大小均对振荡特性有重要影响。随着腔长与深度之比的减小,与最大振荡幅度相对应的振荡频率将移至更高的值。随着腔体后壁角的减小,大多数振荡模式被大大抑制。与陡峭的后壁腔体相反,只有较小的后壁角的腔体的振荡中保留了较高频率的模式。

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