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dc.contributor.authorChandramoorthy, Nisha
dc.contributor.authorWang, Qiqi
dc.date.accessioned2021-11-09T21:57:07Z
dc.date.available2021-11-09T21:57:07Z
dc.date.issued2019-06
dc.identifier.urihttps://hdl.handle.net/1721.1/138090
dc.description.abstract© 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. It is well-known that linearized perturbation methods for sensitivity analysis, such as tangent or adjoint equation-based, finite difference and automatic differentiation are not suitable for turbulent flows. The reason is that turbulent flows exhibit chaotic dynamics, leading to the norm of an infinitesimal perturbation to the state growing exponentially in time. As a result, these conventional methods cannot be used to compute the derivatives of long-time averaged quantities to control or design inputs. The ensemble-based approaches [1, 2] and shadowing-based approaches ([3–5]) to circumvent the problems of the conventional methods in chaotic systems, also suffer from computational impracticality and lack of consistency guarantees, respectively. We introduce the space-split sensitivity, or the S3 algorithm, that is a Monte-Carlo approach to the chaotic sensitivity computation problem. In this work, we derive the S3 algorithm under simplifying assumptions on the dynamics and present a numerical validation on a low-dimensional example of chaos.en_US
dc.language.isoen
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.relation.isversionof10.2514/6.2019-3426en_US
dc.rightsCreative Commons Attribution-Noncommercial-Share Alikeen_US
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/en_US
dc.sourcearXiven_US
dc.titleSensitivity computation of statistically stationary quantities in turbulent flowsen_US
dc.typeArticleen_US
dc.identifier.citationChandramoorthy, Nisha and Wang, Qiqi. 2019. "Sensitivity computation of statistically stationary quantities in turbulent flows." AIAA Aviation 2019 Forum.
dc.contributor.departmentMassachusetts Institute of Technology. Department of Mechanical Engineering
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.relation.journalAIAA Aviation 2019 Forumen_US
dc.eprint.versionAuthor's final manuscripten_US
dc.type.urihttp://purl.org/eprint/type/ConferencePaperen_US
eprint.statushttp://purl.org/eprint/status/NonPeerRevieweden_US
dc.date.updated2021-05-04T18:03:17Z
dspace.orderedauthorsChandramoorthy, N; Wang, Qen_US
dspace.date.submission2021-05-04T18:03:18Z
mit.licenseOPEN_ACCESS_POLICY
mit.metadata.statusAuthority Work and Publication Information Neededen_US


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