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Computational Study of Noise Characteristics for 30P30N Leading-edge Slat and Krueger FlapIn this study, numerical simulations are performed to investigate the flowfield, the noise sources, and their detailed characteristics around high-lift configurations featuring either a conventional leading-edge slat or a Krueger flap. While the flowfields and potential noise sources are similar for the two types of configurations, the noise directivity patterns exhibit some differences. The influence of the cavity where the Krueger flap is stowed on the lower surface is also examined via numerical simulations with and without the cavity. Results show that the cavity does not have a significant influence on the flowfield around the Krueger flap and the gap region. However, when the cavity is present, additional noise sources are observed around its rear part, although they are not as significant as the noise sources on the lower side of the Krueger flap. These additional noise sources contribute to the directivity of high noise levels, especially in the upstream direction.
Document ID
20240005314
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Mitsuhiro Murayama
(Japan Aerospace Exploration Agency Tokyo, Japan)
Kazuomi Yamamoto
(Japan Aerospace Exploration Agency Tokyo, Japan)
Yasushi Ito
(Japan Aerospace Exploration Agency Tokyo, Japan)
Ryotaro Furuya
(Ryoyu Systems Co., Ltd.)
Meelan M Choudhari
(Langley Research Center Hampton, Virginia, United States)
David P Lockard
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
April 29, 2024
Subject Category
Acoustics
Aerodynamics
Meeting Information
Meeting: 30th AIAA/CEAS Aeroacoustics Conference
Location: Rome
Country: IT
Start Date: June 4, 2024
End Date: June 7, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 081876.02.07.15.01.03.01
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
Aeroacoustics
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