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A Requirements-Driven Optimization Method for Acoustic Liners Using Analytic DerivativesMore than ever, there is flexibility and freedom in acoustic liner design. 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. In a previous paper on this subject, a method deriving the ideal target attenuation spectrum that minimizes noise perceived by observers on the ground was described. A simple code-wrapping approach was used to evaluate a community noise objective function for an external optimizer. Gradients were evaluated using a finite difference formula. The subject of this paper is an application of analytic derivatives that supply precise gradients to an optimization process. Analytic derivatives improve the efficiency and accuracy of gradient-based optimization methods and allow consideration of more design variables. In addition, the benefit of variable impedance liners is explored using a multi-objective optimization.
Document ID
20170007696
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Berton, Jeffrey J.
(NASA Glenn Research Center Cleveland, OH United States)
Lopes, Leonard V.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 11, 2017
Publication Date
June 5, 2017
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN42151
Report Number: GRC-E-DAA-TN42151
Meeting Information
Meeting: AIAA/CEAS Aeroacoustics Conference (Aviation Forum 2017)
Location: Denver, CO
Country: United States
Start Date: June 5, 2017
End Date: June 9, 2017
Sponsors: American Inst. of Aeronautics and Astronautics, Council of European Aerospace Societies (CEAS)
Funding Number(s)
WBS: WBS 081876.02.03.30.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Aircraft Noise
Aircraft Engines
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