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Embedded gage impact studyImpact damage in graphite/epoxy laminates was characterized and transient strain history during impact was correlated. The material investigated was AS-4/3501-6 graphite/epoxy. Eight-ply and sixteen-ply quasi-isotropic laminates of 45/0/-45/90 sub s and 45/0/-45/90 sub 2s layups were fabricated with strain gages embedded between plies during the strain gages and leads from the highly conductive graphite fibers. The specimens were circular plates 12.7 cm (5 in.) in diameter and clamped along their circumference. The specimens were impacted with a 185 gm impactor, dropped from heights of 1.20 m and 1.65 m. An accelerometer was attached to the back surface of the specimen opposite the impact point and was used to trigger the recording instrumentation. The transient strain data were recorded with an eight channel waveform digitizer capable of sampling data at 0.5 microsec intervals. The data were stored, processed, and plotted by means of a microcomputer. Transient strain data were correlated with results from ultrasonic inspection of the specimens.
Document ID
19840009490
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Schramm, S. W.
(IIT Research Inst. Chicago, IL, United States)
Daniel, I. M.
(IIT Research Inst. Chicago, IL, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-172227
K06018
NAS 1.26:172227
Report Number: NASA-CR-172227
Report Number: K06018
Report Number: NAS 1.26:172227
Accession Number
84N17558
Funding Number(s)
CONTRACT_GRANT: NAS1-16763
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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