[科技报告]DE  Lockard, D. P., Choudhari, M. M., Buning, P. G.16

摘要: The slat noise from the 30P/30N high-lift system is being investigated through computational fluid dynamics simulations with the OVERFLOW code in conjunction with a Ffowcs Williams-Hawkings acoustics solver. In the present study, ... 展开

翻译摘要
作者 Lockard, D. P.   Choudhari, M. M.   Buning, P. G.  
原报告号 N160005984 总页数 16
主办者 National Aeronautics and Space Administration
报告分类号 [ 46B - Fluid Mechanics, 46A - Acoustics]
报告类别/文献类型 DE / NTIS科技报告
关键词 Boundary conditions   Aerodynamic noise   Aircraft noise   Leading edge slats   Simulation   Ffowcs williams-hawkings equation   Computational fluid dynamics   Computational aeroacoustics   Near fields   Far fields   Acoustics   Noise prediction (aircraft)   Strouhal number   Flow distribution  
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