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Diffraction by Sharp Edges of Noncanonical Shape with Mean Flow and Surface ImpedanceThis paper presents a study on diffraction by sharp edges of noncanonical edge shape in the presence of mean flow and surface impedance, which are important features for aircraft noise but have not been accounted for in previous studies on sharp-edge diffraction. An analytical formula for the diffracted pressure is derived by applying asymptotic analysis to the integral representation of the total pressure scattered by a geometry that contains sharp edges. The asymptotic analysis is presented as a systematic process that can be carried out to any order, if needed. An illustration is given to use a higher-order result to eliminate the singularity in the first-order result to make the solution regular in the entire parameter domain. The formula for the diffracted pressure is validated by experimental data and is applied to parametric studies to reveal the effects of noncanonical edge shape, mean flow and surface impedance, as well as the impact of these effects on the total scattered pressure in the presence of other scattering components.
Document ID
20240004130
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Yueping Guo
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
April 5, 2024
Subject Category
Aircraft Design, Testing and Performance
Meeting Information
Meeting: AIAA 30th 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: 081876.02.07.30.10.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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