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Prediction of Flow Dynamics over Cavities by Detached Eddy Simulation

机译:用分离涡模拟预测腔内流动动力学。

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摘要

In this investigation, the flow simulation over different types of cavities (two- and three-dimensional) wasnperformed. The effect of turbulence was implemented with detached-eddy simulation using the Spalart–Allmarasnone-equation model. Initially, the flow behavior was investigated and compared for open and closed cavities. In thensound pressure level spectra of the closed cavity, only the broadband noise can be observed, while in the open-cavityncase, it consisted of harmonic frequency peaks. Results of the two- and three-dimensional computations werencompared with each other and with the available experimental data. It was observed that the results of three-ndimensional simulations comparedwellwith the experimental data, and the amplitude of the pressure fluctuations innthe two-dimensional case was larger than in the three-dimensional model.Moreover, the pressure fluctuation of thentwo-dimensional cavity was more periodic than that of the three-dimensional case. Subsequently, a cavity with twoncircular openings on top, representing a landing gear housing, was investigated. Results show that the existence ofnthese openings changes the characteristics of the flow inside the cavity, and the computed frequencies differ fromthenresults calculated by the Rossiter semi-empirical formula.
机译:在这项研究中,对不同类型的腔体(二维和三维)进行了流动仿真。湍流的影响通过使用Spalart-Allmarasn​​one方程模型的独立涡流模拟实现。最初,研究了流动行为,并比较了开放腔和封闭腔的流动特性。在封闭腔的声压级谱中,只能观察到宽带噪声,而在开放腔的情况下,它由谐波频率峰值组成。二维和三维计算的结果彼此之间以及可用的实验数据上都没有进行比较。可以看出,三维模拟的结果与实验数据相比较,二维情况下的压力波动幅度要大于三维模型中的波动幅度,而且二维空腔的压力波动幅度更大。周期性的比三维的情况。随后,研究了在顶部具有两个圆形开口的空腔,它们代表起落架壳体。结果表明,这些开孔的存在改变了空腔内部流动的特性,计算出的频率与通过Rossiter半经验公式计算出的结果有所不同。

著录项

  • 来源
    《Journal of Aircraft》 |2010年第6期|p.1991-2004|共14页
  • 作者单位

    Wichita State University, Wichita, Kansas 67260-0044;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 23:06:13

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