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Applications of diffraction theory to aeroacousticsThe fundamentals of diffraction theory were reviewed and applied to several problems of aircraft noise generation, propagation, and measurement. The general acoustic diffraction problem is defined and the governing equations were set down. Diffraction phenomena are illustrated using the classical problem of the diffraction of a plane wave by a half-plane. Infinite series and geometric acoustic methods for solving diffraction problems are described. Four applications of diffraction theory are discussed: the selection of an appropriate shape for a microphone, the use of aircraft wings to shield the community from engine noise, the reflection of engine noise from an aircraft fuselage, and the radiation of trailing edge noise.
Document ID
19800006612
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lansing, D. L.
(NASA Langley Research Center Hampton, VA, United States)
Liu, C. H.
(NASA Langley Research Center Hampton, VA, United States)
Norum, T. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
August 1, 1979
Publication Information
Publication: AGARD Special Course on Acoustic Wave Propagation
Subject Category
Acoustics
Accession Number
80N14870
Distribution Limits
Public
Copyright
Other
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