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A Requirements-Driven Optimization Method for Acoustic Treatment DesignAcoustic treatment designers are able to attenuate specific noise sources inside turbofan engines. Subject to practical considerations, liner design variables may be manipulated to achieve a target attenuation spectrum. But, characteristics of the ideal attenuation spectrum can be difficult to know. Many multidisciplinary system effects govern how engine noise sources contribute to community noise. Given a hardwall fan noise source to be suppressed, and using an analytical certification noise model to compute a community noise measure of merit, the optimal attenuation spectrum can be derived using multidisciplinary systems analysis methods. The subject of this paper is an analytic method that derives the ideal target attenuation spectrum that minimizes noise perceived by observers on the ground. Software is developed and used to test and validate the method on a simple, notional source. With experience gained from minimizing noise of the simple source, the software is tested against a realistic hardwall fan source.
Document ID
20220013661
Acquisition Source
Glenn Research Center
Document Type
Accepted Manuscript (Version with final changes)
Authors
Jeffrey J. Berton
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
September 6, 2022
Publication Date
May 18, 2017
Publication Information
Publication: Journal of Aircraft
Publisher: American Institute of Aeronautics and Astronautics
Volume: 54
Issue: 6
Issue Publication Date: November 1, 2017
ISSN: 0021-8669
e-ISSN: 1533-3868
Subject Category
Acoustics
Funding Number(s)
WBS: 081876.02.03.30.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
aircraft noise
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