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Vibration testing of impact-damaged composite laminatesA new test is described that can be used to measure changes in the vibration properties of impact damaged composite materials. Impact-induced delamination was observed to significantly affect natural frequencies of vibration and damping properties in cross-ply graphite/epoxy laminates. Natural frequencies are shown to drop by as much as half of their original value, and modal damping ratios can increase by a factor of up to eight when large amounts of damage are present. A simple finite element model of the damaged impact specimens was used to predict the effect of delamination on certain vibration properties. A comparison of the finite element calculations with the experimental measurements suggests that delamination was the dominant mechanism of flexural stiffness loss resulting from the transverse impact.
Document ID
19890015919
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Grady, Joseph E.
(NASA Lewis Research Center Cleveland, OH, United States)
Meyn, Erwin H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1989
Subject Category
Composite Materials
Report/Patent Number
E-4518
NAS 1.15:4115
NASA-TM-4115
Report Number: E-4518
Report Number: NAS 1.15:4115
Report Number: NASA-TM-4115
Meeting Information
Meeting: Structures, Structural Dynamics and Materials Conference
Location: Mobile, AL
Country: United States
Start Date: April 3, 1989
End Date: April 5, 1989
Sponsors: AIAA, AHS, ASCE, ASME, ASC
Accession Number
89N25290
Funding Number(s)
PROJECT: RTOP 505-63-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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