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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Low-Order Modeling of Combustion Noise in an Aero-Engine: The Effect of Entropy Dispersion
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Low-Order Modeling of Combustion Noise in an Aero-Engine: The Effect of Entropy Dispersion

机译:航空发动机燃烧噪声的低阶建模:熵扩散的影响

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摘要

The present work studies the effect of entropy dispersion on the level of combustion noise at the turbine outlet of the Rolls-Royce ANTLE aero-engine. A new model for the decay of entropy waves, based on modeling dispersion effects, is developed and utilized in a low-order network model of the combustor (i.e., LOTAN code that solves the unsteady Euler equations). The proposed model for the dispersion of entropy waves only requires the mean velocity field as an input, obtained by Reynolds-averaged Navier-Stokes (RANS) computations of the demonstrator combustor. LOTAN is then coupled with a low-order model code (LINEARB) based on the semi-actuator disk model that studies propagation of combustion noise through turbine blades. Thus, by combining LOTAN and LINERAB, the combustion noise and its counterparts, direct and indirect noise, generated at the turbine exit are predicted. In comparison with experimental data, it is found that without the inclusion of entropy dispersion, the level of combustion noise at the turbine exit is overpredicted by almost 2 orders of magnitude. The introduction of entropy dispersion in LOTAN results in a much better agreement with the experimental data, highlighting the importance of entropy wave dispersion for the prediction of combustion noise in real engines. In more detail, the agreement with the experiment for high and low frequencies was very good. At intermediate frequencies, the experimental measurements are still overpredicted; however, the predicted noise is much smaller compared to the case without entropy dispersion. This discrepancy is attributed to (i) the role of turbulent mixing in the overall decay of the entropy fluctuations inside the combustor, not considered in the model developed for the decay of entropy waves, and (ii) the absence of a proper model in LINEARB for the decay of entropy waves as they pass through the turbine blade rows. These are areas that still need further development to improve the prediction of low-order network codes.
机译:本工作研究了劳斯莱斯ANTLE航空发动机的涡轮出口处的熵散对燃烧噪声水平的影响。基于建模弥散效应,开发了一种用于熵波衰减的新模型,并将其用于燃烧器的低阶网络模型(即解决不稳定Euler方程的LOTAN代码)。所提出的用于熵波扩散的模型仅需要平均速度场作为输入,该速度是通过演示燃烧器的雷诺平均Navier-Stokes(RANS)计算获得的。然后,将LOTAN与基于半致动器盘模型的低阶模型代码(LINEARB)耦合,该模型研究燃烧噪声通过涡轮叶片的传播。因此,通过组合LOTAN和LINERAB,可以预测在涡轮机出口处产生的燃烧噪声及其对应的直接和间接噪声。与实验数据相比,发现在不包括熵扩散的情况下,涡轮出口处的燃烧噪声水平被高估了将近2个数量级。在LOTAN中引入熵扩散可以更好地与实验数据相吻合,从而突出了熵波扩散对预测真实发动机燃烧噪声的重要性。更详细地说,与高频和低频实验的一致性很好。在中频处,实验测量值仍然被高估了。然而,与没有熵扩散的情况相比,预测的噪声要小得多。这种差异归因于(i)湍流混合在燃烧器内部熵波动的整体衰减中的作用,而在为熵波衰减而开发的模型中未考虑该因素,以及(ii)LINEARB中缺少合适的模型熵波在通过涡轮叶片排时的衰减。这些领域仍需要进一步发展以改善对低阶网络代码的预测。

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  • 来源
    《Journal of Engineering for Gas Turbines and Power》 |2018年第1期|011502.1-011502.7|共7页
  • 作者单位

    Department of Engineering, University of Cambridge, Trumpington Street, Cambridge CB2 1PZ, UK;

    Department of Engineering, University of Cambridge, Trumpington Street, Cambridge CB2 1PZ, UK;

    Department of Engineering, University of Cambridge, Trumpington Street, Cambridge CB2 1PZ, UK;

    Department of Engineering, University of Cambridge, Trumpington Street, Cambridge CB2 1PZ, UK;

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