Flight Demonstrator of a Self-Powered SHM System on a Composite Bonded Patch Attached to an F/A-18 Aileron Hinge

dc.contributor.authorGalea, S. C.en_US
dc.contributor.authorVelden, S.en_US
dc.contributor.authorPowlesland, I.en_US
dc.contributor.authorNguyen, Q.en_US
dc.contributor.authorFerrarotto, P.en_US
dc.contributor.authorKonak, M.en_US
dc.date.accessioned2014-05-09T07:09:43Z
dc.date.available2014-05-09T07:09:43Z
dc.date.issued2006-12en_US
dc.identifier.citationAsia-Pacific Workshop on Structural Health Monitoring, Dec. 4-6 2006, Yokohama Japan, p. 146-154.en_US
dc.identifier.urihttp://iroha.scitech.lib.keio.ac.jp:8080/sigma/handle/10721/2695
dc.languageenen_US
dc.rights.holderAkira Mita Laboratory, Faculty of Science and Technology, Keio University, Yokohama, Japan.en_US
dc.titleFlight Demonstrator of a Self-Powered SHM System on a Composite Bonded Patch Attached to an F/A-18 Aileron Hingeen_US
dc.typeArticleen_US

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