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dc.contributor.authorChakravarthy, Animesh
dc.contributor.authorEvans, Katie A.
dc.contributor.authorKuhn, Lisa M.
dc.contributor.authorWalters, Jonathan B.
dc.identifier.citationChakravarthy, Animesh; Evans, Katie A.; Kuhn, Lisa M.; Walters, Jonathan B. 2015. Frequency and time domain analysis of an aeroelastic wing multiple component structure. Numerical Functional Analysis and Optimization, vol. 36:no. 9:pp 1122-1152en_US
dc.descriptionClick on the DOI link to access the article (may not be free).en_US
dc.description.abstractA multiple component structure consisting of two Euler-Bernoulli beams connected to a rigid mass is used to model the heave dynamics of a wing micro air vehicle. In the time domain, the attainment of a Cₒ-semigroup in the context of sesquilinear forms is demonstrated. In addition, the closed loop system is demonstrated to generate an exponentially stable Cₒ-semigroup. In the frequency domain, the infinite dimensional transfer function is determined and used to examine several properties of the system. Finally, an optimal control is used to morph the wings to a desired shape, and simulation results are demonstrated.en_US
dc.description.sponsorshipNASA Research Infrastructure Development (RID) Grant NNX13AB11A.en_US
dc.publisherTaylor & Francis Groupen_US
dc.relation.ispartofseriesNumerical Functional Analysis and Optimization;v.36:no.9
dc.subjectFlexible wingsen_US
dc.subjectInfinite dimensional transfer functionen_US
dc.subjectMicro air vehicleen_US
dc.subjectMultiple component structureen_US
dc.titleFrequency and time domain analysis of an aeroelastic wing multiple component structureen_US
dc.rights.holder© Informa UK Limited, an Informa Group Companyen_US

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    Research publications authored by the Department of Aerospace Engineering faculty and graduate students.

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