边界层
湍流
机械
声学
流动分离
航空航天工程
物理
工程类
作者
Teresa S. Miller,Judith M. Gallman,Mark J. Moeller
出处
期刊:Journal of Aircraft
[American Institute of Aeronautics and Astronautics]
日期:2012-11-01
卷期号:49 (6): 1739-1754
被引量:46
摘要
A survey of the available turbulent boundary layer models for acoustic analysis is presented. The empirical mean square pressure models predict a relatively large spread in the values; bounded on the high end by Kraichnan and on the low end by Bull, and Willmarth and Wooldridge. The single point wall pressure spectrum models are evaluated and the two more modern models of Smol’yakov and Goody seem to perform the best. Important features of the normalized wavenumber-frequency spectrum models are presented. Separable models in the Corcos class tend to over-predict the response for a range of cases.
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