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Modeling unsteadiness in steady simulations with neural network generated lumped deterministic source terms.

机译:使用神经网络在稳定模拟中对不稳定进行建模会生成集总的确定性源项。

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摘要

The lumped deterministic source term—neural network (LDST-NN) approach has been developed to obtain quasi-time-average solutions of cavity flows that include unsteady cavity effects in steady-state computations without the cavity. The results obtained with the LDST-NN based steady calculations are compared to the time average of fully unsteady solutions via the shear force acting on the cavity walls. Two orders of magnitude less computational time is required to obtain a quasi-time average simulation relative to time accurate simulations; a substantial savings. The estimated error, based on the calculated drag force, in these simulations is between 4% and 15% as compared to fully unsteady calculations, which is satisfactory for many design purposes. This should be compared to the 40% to 154% errors obtained by neglecting the cavity completely for these same cases. As such, the modified neural network-based LDST model is a viable tool for representing unsteady cavity effects. The LDST-NN quasi-time averaged solution was able to capture global unsteady effects correctly.; The LDSTs were found to correlate directly with observed sound pressure level trends and provide an additional means of assessing unsteadiness. The LDSTs were found to reach a maximum near the cavity/main flow interface but also extended well into the field; indicating that boundary condition representations alone would be inadequate for capturing unsteady effects.; Deterministic source terms were computed from unsteady simulations and modeled with a neural network for use in steady simulations sans cavity to capture the entire time average effect of the cavity. This was demonstrated for the entire range of Mach numbers, length-to-depth ratios and various translational velocities of the cavity wall.; The results of the study showed that modeling flow over cavities is possible with steady simulations that include source terms provided by a neural network. This method permits a considerable reduction in CPU time and is attractive for large scale simulations since it includes the effects of the unsteady phenomena without computing the unsteady flow inside the cavity.
机译:已经开发了集总的确定性源项-神经网络(LDST-NN)方法来获得空腔流动的准时间平均解,其中在没有空腔的稳态计算中包括非稳态空腔效应。通过基于腔壁的剪切力,将基于LDST-NN的稳态计算获得的结果与完全非稳态解的时间平均值进行比较。相对于时间准确的仿真,获得准时间平均仿真所需的计算时间少两个数量级;大量节省。与完全不稳定的计算相比,这些模拟中基于计算出的阻力的估计误差在4%到15%之间,这对于许多设计目的都是令人满意的。这应该与在相同情况下完全忽略型腔所获得的40%至154%的误差相比较。因此,基于神经网络的修改后的LDST模型是一种用于表示不稳定腔效应的可行工具。 LDST-NN准时平均解决方案能够正确捕获全局不稳定影响。发现LDST与观察到的声压级趋势直接相关,并提供了评估不稳定的另一种方法。发现LDST在腔/主流界面附近达到最大值,但也很好地延伸到了现场。表明仅边界条件表示不足以捕获不稳定的影响。确定性源项是通过非稳态模拟计算得出的,并使用神经网络进行建模,用于无腔稳态模拟,以捕获腔的整个时间平均效应。在整个马赫数范围,长深比和腔壁的各种平移速度方面得到了证明。研究结果表明,通过包括神经网络提供的源项在内的稳定模拟,可以对型腔上的流动进行建模。该方法可显着减少CPU时间,并且对于大规模仿真具有吸引力,因为该方法包括不稳定现象的影响,而无需计算腔体内的不稳定流量。

著录项

  • 作者

    Lukovic, Bojan.;

  • 作者单位

    University of Cincinnati.;

  • 授予单位 University of Cincinnati.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2002
  • 页码 200 p.
  • 总页数 200
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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