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Rudimentary landing gear results at the 2012 BANC-II airframe noise workshop

机译:基本起落架在2012年BANC-II机体噪声研讨会上的成果

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The results of large-eddy and similar simulations and acoustic propagation calculations provided by six participants for the Rudimentary Landing Gear (RLG) category of the 2012 BANC-II workshop are analyzed and compared with experimental results. The general conclusion is that industrial accuracy remains elusive, and very significant differences exist between methods, so that the field needs more maturity, in addition to computing power. We present both blind comparisons from the workshop, and revised results the participants were invited to provide after having access to the experimental data. We recall that BANC-I and other comparisons indicate good code-to-code and experimental agreement for time-averaged pressures, but not so much for unsteady pressures and forces. Possibly as a result of these differences, the agreement for radiated noise is quite poor in the blind test, with typical differences of over 5 dB for the SPL and for the spectra over the dominant frequency range, and reaching 10 dB towards both ends of the spectra. The collection of numerical results brackets the experimental result. Some differences arise from misunderstandings, which were not corrected. The post-workshop results are much closer to experiment, with differences reduced to about 3 dB for SPL, and for spectra up to a Strouhal number of 15. This is not up to industrial needs, but is very encouraging and close to the accuracy achieved for jet noise. The results are sensitive to the use of solid or permeable surfaces in the Ffowcs Williams-Hawkings (FW-H) equation, and to numerous simulation details such as upwind-biased differencing.
机译:分析了由六名参与者为2012 BANC-II研讨会的基本起落架(RLG)类别提供的大涡流和类似模拟的结果以及声传播计算的结果,并将其与实验结果进行了比较。总的结论是,工业精度仍然难以捉摸,并且方法之间存在非常显着的差异,因此,除了计算能力外,该领域还需要更成熟。我们提供了来自研讨会的盲目比较,以及访问实验数据后邀请参与者提供的修改结果。我们记得,BANC-I和其他比较表明时间平均压力具有良好的代码对代码和实验一致性,但对于不稳定的压力和作用力则没有那么多。这些差异的可能结果是,在盲测中辐射噪声的一致性非常差,SPL和主要频率范围内的频谱的典型差异超过5 dB,并且在频谱两端均达到10 dB。光谱。数值结果的集合括在实验结果中。误解引起了一些差异,这些差异没有得到纠正。车间后的结果更接近于实验,对于SPL和最大Strouhal数为15的光谱,差异减小到大约3 dB。这不符合工业需求,但是非常令人鼓舞,并且接近达到的精度喷射噪音。该结果对于在Ffowcs Williams-Hawkings(FW-H)方程中使用固体或渗透性表面以及许多模拟细节(如迎风偏微分)敏感。

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