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Numerical analysis of the aerodynamic noise prediction in Direct Numerical Simulation and Large Eddy Simulation

机译:直接数值模拟和大涡模拟中空气动力学噪声预测的数值分析

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摘要

This thesis presents the rigorous numerical analysis of the aerodynamic noise generation viaLighthill acoustic analogy, which is a non-homogeneous wave equation describing thesound waves. Over more than five decades, the Lighthill analogy was extensively used as oneof the major tools in engineering applications in acoustics. However, the first mathematicalresearch of the Finite Element approximation for it is introduced here. Specifically, we focuson both Direct Numerical and Large Eddy Simulations. The more or less intuitive derivationof the Lighthill analogy is reviewed in section 1.3.First, the semidiscrete and fully discrete Finite Element methods in DNS are presentedand the effect of the computational error in the right-hand side of the wave equation ispointed out. The convergence of this error to zero is studied in the semidiscrete case. Thecomputational results support obtained theoretical predictions.Second, the numerical analysis, using the negative norms of the error, is presented in thesemidiscrete case. The negative norms help obtain better convergence rate and require lessregularity of the data than positive norms.Third, the sound power is defined as a non-linear functional of acoustic variables andthree independent ways of computing it in the semidiscrete case in DNS are presented. Allof these methods are based on the Finite Element scheme presented earlier. The methodsare compared from the point of view of computational cost, accuracy and simplicity. Again,the computational experiments are presented.Finally, the concept of Large Eddy Simulation is introduced for aeroacoustic researchvia Lighthill analogy. Two subgrid scale models, these are van Cittert deconvolution andBardina, are presented for the filtered acoustic analogy. The semidiscrete Finite ElemetMethod is analyzed for both of them. We present the numerical experiments for this researchas well.
机译:本文通过Lighthill声学类比对空气动力噪声的产生进行了严格的数值分析,这是一个非均匀波方程,描述了声波。在超过五十年的时间里,Lighthill类比被广泛用作声学工程应用中的主要工具之一。但是,这里介绍了对其进行有限元近似的第一次数学研究。具体来说,我们专注于直接数值模拟和大涡模拟。在第1.3节中回顾或多或少地直观地推导出了Lighthill类推。首先,提出了DNS中的半离散和全离散有限元方法,并指出了波动方程右侧的计算误差的影响。在半离散情况下研究了该误差为零的收敛性。计算结果支持了所获得的理论预测。其次,在这种中等程度的情况下,利用误差的负范数进行了数值分析。与正规范相比,负规范有助于获得更好的收敛速度,并且需要更少的数据规则性。第三,声功率被定义为声学变量的非线性函数,并且在DNS的半离散情况下提出了三种独立的计算方法。所有这些方法都是基于前面介绍的有限元方案。从计算成本,准确性和简单性的角度比较了这些方法。再次,给出了计算实验。最后,通过Lighthill类比将大涡模拟的概念引入航空声学研究。提出了两个子网格规模模型,分别是van Cittert反卷积模型和Barardina模型,用于滤波后的声学类比。对半离散有限Elemet方法进行了分析。我们也为这项研究提供了数值实验。

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