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Helicopter Performance and Vibration Enhancement by Twist-Actuated Blades
dc.contributor.authorShin, Sangjoonen_US
dc.contributor.authorCesnik, Carlos E. S.en_US
dc.date.accessioned2010-06-11T19:18:04Z
dc.date.available2010-06-11T19:18:04Z
dc.date.issued2003en_US
dc.identifier.citationShin, Sangjoon; Cesnik, Carlos (2003). "Helicopter Performance and Vibration Enhancement by Twist-Actuated Blades" AIAA-2003-1818, 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Norfolk, Virginia, Apr. 7-10, 2003. <http://hdl.handle.net/2027.42/77375>en_US
dc.identifier.otherAIAA-2003-1818en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/77375
dc.format.extent613096 bytes
dc.format.extent3112 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypetext/plain
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleHelicopter Performance and Vibration Enhancement by Twist-Actuated Bladesen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumUniversity of Michigan, Ann Arbor, MIen_US
dc.contributor.affiliationumUniversity of Michigan, Ann Arbor, MIen_US
dc.identifier.pmid14673586en_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/77375/1/AIAA-2003-1818-349.pdf
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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