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Free edge strain concentrations in real composite laminates Experimental-theoretical correlationThe magnitude of the maximum shear strain at the free edge of axially loaded theta (2)/theta(2)(s) and (+ or - theta(2) (s) composite laminates was investigated experimentally and numerically to ascertain the actual value of strain concentration in resin matrix laminates and to determine the accuracy of finite element results. Experimental results using moire interferometry show large, but finite, shear strain concentrations at the free edge of graphite-epoxy and graphite-polyimide laminates. Comparison of the experimental results with those obtained using several different finite element representations showed that a four node isoparametric finite element provided the best and most trouble free numerical results. The results indicate that the ratio of maximum shear strain at the free edge to applied axial strain varies with fiber orientation and does not exceed nine for the most critical angle which is 15 deg.
Document ID
19860034047
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Herakovich, C. T.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Post, D.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Buczek, M. B.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Czarnek, R.
(Virginia Polytechnic Institute and State University Blacksburg, United States)
Date Acquired
August 12, 2013
Publication Date
December 1, 1985
Publication Information
Publication: ASME, Transactions, Journal of Applied Mechanics
Volume: 52
ISSN: 0021-8936
Subject Category
Structural Mechanics
Report/Patent Number
ASME PAPER 85-WA/APM-10
Accession Number
86A18785
Funding Number(s)
CONTRACT_GRANT: NSF MEA-81-09230
CONTRACT_GRANT: NCC1-15
Distribution Limits
Public
Copyright
Other

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