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The multidisciplinary design of aircraft typically includes considerations of performance, weight, fuel burn, and noise, among other factors. This document will present an approach for defining the sensitivity of several acoustic metrics and operations that can fill the role of the acoustic function.

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This page is a summary of: Robust Acoustic Objective Functions and Sensitivities in Adjoint-Based Design Optimizations, AIAA Journal, August 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j056518.
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