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Dymore Finite Element Analysis Of The Paired Blade Tiltrotor Conceptual Design And A Comparable Conventional Tiltrotor Design

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Dymore Finite Element Analysis Of The Paired Blade Tiltrotor Conceptual Design And A Comparable Conventional Tiltrotor Design

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dc.contributor.author Braziel, David Orion en_US
dc.date.accessioned 2009-09-16T18:16:52Z
dc.date.available 2009-09-16T18:16:52Z
dc.date.issued 2009-09-16T18:16:52Z
dc.date.submitted January 2009 en_US
dc.identifier.other DISS-10208 en_US
dc.identifier.uri http://hdl.handle.net/10106/1661
dc.description.abstract Increasing 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.sponsorship Lawrence, Kent en_US
dc.language.iso EN en_US
dc.publisher Aerospace Engineering en_US
dc.title Dymore Finite Element Analysis Of The Paired Blade Tiltrotor Conceptual Design And A Comparable Conventional Tiltrotor Design en_US
dc.type M.S. en_US
dc.contributor.committeeChair Lawrence, Kent en_US
dc.degree.department Aerospace Engineering en_US
dc.degree.discipline Aerospace Engineering en_US
dc.degree.grantor University of Texas at Arlington en_US
dc.degree.level masters en_US
dc.degree.name M.S. en_US
dc.identifier.externalLink http://www.uta.edu/ra/real/editprofile.php?onlyview=1&pid=256
dc.identifier.externalLinkDescription Link to Research Profiles

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