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
作者 | Lockard, D. P. Choudhari, M. M. Buning, P. G. | ||
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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 |