@inproceedings{5886aec9c0bb4216ab0c5884b8852a9c,
title = "A discrete adjoint-based shape optimization for shear-layer-noise reduction",
abstract = "A discrete-exact adjoint-based optimization is used to adjust a wall shape to reduce the noise of an adjacent spatially developing compressible shear layer. For high-fidelity predictive simulations of this kind, a {\textquoteleft}trial-and-error{\textquoteright} approach to minimize a quantity of interest is prohibitively expensive for high-dimensional control spaces. Adjoint-based methods can point the direction of optimal shape with respect to an arbitrarily large number of control parameters at approximately the same computational cost as a single predictive simulation. A key aspect of this space-time discrete-adjoint method is that the gradient is exact to the numerical precision of the calculation. With the discrete exact gradient, we obtain a noise reduction of ˇ 2.5 dB in our model flow with a Fourier-based wall shape parametrization for a compressible near-wall spatially developing shear layer. We demonstrate that the gradient is exact up to machine precision.",
author = "Buchta, {David A.} and Ramanathan Vishnampet and Bodony, {Daniel J.} and Freund, {Jonathan B.}",
note = "Publisher Copyright: {\textcopyright} 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 22nd AIAA/CEAS Aeroacoustics Conference, 2016 ; Conference date: 30-05-2016 Through 01-06-2016",
year = "2016",
doi = "10.2514/6.2016-2776",
language = "English (US)",
isbn = "9781624103865",
series = "22nd AIAA/CEAS Aeroacoustics Conference, 2016",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "22nd AIAA/CEAS Aeroacoustics Conference",
}