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dc.contributor.authorBraziel, David Orionen_US
dc.date.accessioned2009-09-16T18:16:52Z
dc.date.available2009-09-16T18:16:52Z
dc.date.issued2009-09-16T18:16:52Z
dc.date.submittedJanuary 2009en_US
dc.identifier.otherDISS-10208en_US
dc.identifier.urihttp://hdl.handle.net/10106/1661
dc.description.abstractIncreasing the solidity of tiltrotors above that of current designs presents challenges associated with control system packaging and control couplings. The paired blade rotor concept addresses these issues by placing two blades that share a pitch link, located for acceptable control coupling, on each of three hub arms.Dymore finite element models of the paired blade rotor and a reference rotor of equal solidity with six evenly spaced blades were developed to identify any potential design flaws of the paired blade rotor associated with rotor frequency placement or control couplings. The finite element rotor models are documented, and the results of the analyses are presented here.en_US
dc.description.sponsorshipLawrence, Kent L.en_US
dc.language.isoENen_US
dc.publisherAerospace Engineeringen_US
dc.titleDymore Finite Element Analysis Of The Paired Blade Tiltrotor Conceptual Design And A Comparable Conventional Tiltrotor Designen_US
dc.typeM.S.en_US
dc.contributor.committeeChairLawrence, Kent L.en_US
dc.degree.departmentAerospace Engineeringen_US
dc.degree.disciplineAerospace Engineeringen_US
dc.degree.grantorUniversity of Texas at Arlingtonen_US
dc.degree.levelmastersen_US
dc.degree.nameM.S.en_US
dc.identifier.externalLinkhttp://www.uta.edu/ra/real/editprofile.php?onlyview=1&pid=256
dc.identifier.externalLinkDescriptionLink to Research Profiles


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