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Effects of Delaminations on the Damped Dynamic Characteristics of Composite Laminates: Mechanics and ExperimentsAnalytical and experimental work is presented on the damped free-vibration of delaminated laminates and beams. A laminate theory is developed where the unknown kinematic perturbations induced by a delamination crack are treated as additional degrees of freedom. The generalized stiffness, inertia and damping matrices of the laminate are formulated. An analytical solution is developed for the prediction of natural frequencies, modes and modal damping in composite beams with delamination cracks. Evaluations of the mechanics on various cantilever beams with a central delamination are performed. Experimental results for the modal frequencies and damping of composite beams with a single delamination are also presented and correlations between analytical predictions and measured data are shown. The effects of delamination vary based on crack size, laminate configuration, and mode order. The implications of the mechanics in developing delamination detection techniques are also discussed.
Document ID
19950016838
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Saravanos, D. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Hopkins, D. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1995
Subject Category
Composite Materials
Report/Patent Number
E-9467
NAS 1.15:106862
NASA-TM-106862
Report Number: E-9467
Report Number: NAS 1.15:106862
Report Number: NASA-TM-106862
Accession Number
95N23258
Funding Number(s)
PROJECT: RTOP 505-63-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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