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Predictions of Slat Noise from the 30P30N at High Angles of Attack Using Zonal Hybrid RANS-LESAeroacoustic predictions of slat noise from the 30P30N three-element high-lift system at high angles of attack are presented using a zonal hybrid RANS-LES method. The simulations are part of the 5th AIAA Benchmark problems for Airframe Noise Computations (BANC-V) Workshop. An economical approach utilizing structured overset grids with spatially varying span-wise grid resolution and a high-order accurate finite difference method is described. The method is utilized for near-field predictions at three angles of attack: α = 5.5, 9.5, and 14.0 degrees. Far-field noise is obtained by propagating the near-field solution using a permeable surface Ffowcs Williams-Hawkings (FWH) method. Good agreement is obtained with both near-field and far-field Power Spectral Density (PSD) data from an experimental study of the 30P30N in the 2m x 2m Kevlar-wall wind tunnel at the Japan Aerospace Exploration Agency (JAXA). Specifically, the reduction in narrow band peaks and overall broadband noise levels with increasing angle of attack is captured well using the zonal hybrid RANS-LES method.
Document ID
20190030756
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Housman, Jeffrey A.
(NASA Ames Research Center Moffett Field, CA, United States)
Stich, Gerrit-Daniel
(Science and Technology Corp. Moffett Field, CA, United States)
Kiris, Cetin
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 12, 2019
Publication Date
May 20, 2019
Subject Category
Acoustics
Report/Patent Number
ARC-E-DAA-TN68792
Meeting Information
Meeting: AIAA/CEAS Aeroacoustics Conference (Aeroacoustics 2019)
Location: Delft
Country: Netherlands
Start Date: May 20, 2019
End Date: May 23, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
CONTRACT_GRANT: NNA16BD60C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
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