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dc.contributor.authorRokhsaz, Kamran
dc.contributor.authorKliment, Linda K.
dc.date.accessioned2019-04-26T13:37:25Z
dc.date.available2019-04-26T13:37:25Z
dc.date.issued2018-11-12
dc.identifier.citationHigher-Order Estimations of Load Factor from Derived Gust Velocity Kamran Rokhsaz and Linda K. Kliment Journal of Aircraft 2019 56:2, 591-596en_US
dc.identifier.issn0021-8669
dc.identifier.urihttps://doi.org/10.2514/1.C034977
dc.identifier.urihttp://hdl.handle.net/10057/16130
dc.descriptionClick on the DOI link to access the article (may not be free).en_US
dc.description.abstractPratt's formula, in which the aircraft is modeled as a single-degree-of-freedom system, is used extensively to extract derived gust velocities from measured normal acceleration. There is evidence that airframe mass distribution along the longitudinal axis can affect the gust load alleviation factor. In this paper, the inclusion of the pitching degree of freedom in the model is explored, accounting for the aircraft mass distribution along the longitudinal axis. Two different two-degree-of-freedom models are presented and numerical solutions are offered. A typical heavy transport aircraft is used for illustration. It is shown that the inclusion of the second degree of freedom results in as much as 10% reduction in the magnitude of the gust load alleviation factor.en_US
dc.language.isoen_USen_US
dc.publisherAmerican Institute of Aeronautics and Astronautics, Inc.en_US
dc.relation.ispartofseriesJournal of Aircraft;v.56:no.2
dc.subjectAircraften_US
dc.subjectAtmospheric turbulenceen_US
dc.titleHigher-order estimations of load factor from derived gust velocityen_US
dc.typeConference paperen_US
dc.rights.holder© 2018 by the authorsen_US


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

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