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Damage progression in compressively loaded laminates containing a circular cutout
dc.contributor.authorWaas, Anthony M.en_US
dc.contributor.authorKnauss, W. G.en_US
dc.contributor.authorBabcock, C. D.en_US
dc.date.accessioned2010-06-11T17:50:28Z
dc.date.available2010-06-11T17:50:28Z
dc.date.issued1991en_US
dc.identifier.citationWaas, A. M.; Knauss, W. G.; Babcock, C. D., (1991). "Damage progression in compressively loaded laminates containing a circular cutout" AIAA Journal, vol.29 no.3 (436-443). <http://hdl.handle.net/2027.42/76038>en_US
dc.identifier.issn0001-1452en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/76038
dc.format.extent2072817 bytes
dc.format.extent3112 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypetext/plain
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleDamage progression in compressively loaded laminates containing a circular cutouten_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumMichigan, University, Ann Arboren_US
dc.contributor.affiliationotherCalifornia Institute of Technology, Pasadenaen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/76038/1/AIAA-10597-113.pdf
dc.identifier.doi10.2514/3.10597en_US
dc.identifier.sourceAIAA Journalen_US
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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