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Influence of Spanwise Boundary Conditions on Slat Noise SimulationsThe 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, two different spanwise grids are being used to investigate the effect of the spanwise extent and periodicity on the near-field unsteady structures and radiated noise. The baseline grid with periodic boundary conditions has a short span equal to 1/9th of the stowed chord, whereas the other, longer span grid adds stretched grids on both sides of the core, baseline grid to allow inviscid surface boundary conditions at both ends. The results indicate that the near-field mean statistics obtained using the two grids are similar to each other, as are the directivity and spectral shapes of the radiated noise. However, periodicity forces all acoustic waves with less than one wavelength across the span to be two-dimensional, without any variation in the span. The spanwise coherence of the acoustic waves is what is needed to make estimates of the noise that would be radiated from realistic span lengths. Simulations with periodic conditions need spans of at least six slat chords to allow spanwise variation in the low-frequencies associated with the peak of broadband slat noise. Even then, the full influence of the periodicity is unclear, so employing grids with a fine, central region and highly stretched meshes that go to slip walls may be a more efficient means of capturing the spanwise decorrelation of low-frequency acoustic phenomena.
Document ID
20160005984
Acquisition Source
Langley Research Center
Document Type
Conference Paper
External Source(s)
Authors
Lockard, David P.
(NASA Langley Research Center Hampton, VA, United States)
Choudhari, Meelan M.
(NASA Langley Research Center Hampton, VA, United States)
Buning, Pieter G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
May 10, 2016
Publication Date
June 22, 2015
Subject Category
Acoustics
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-20034
AIAA Paper 2015-3136
Report Number: NF1676L-20034
Report Number: AIAA Paper 2015-3136
Meeting Information
Meeting: AIAA Aviation
Location: Dallas, TX
Country: United States
Start Date: June 22, 2015
End Date: June 26, 2015
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 473452.02.07.07.03.01.05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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