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Prediction of impact force and duration during low velocity impact on circular composite laminatesTwo simple and improved models--energy-balance and spring-mass--were developed to calculate impact force and duration during low velocity impact of circular composite plates. Both models include the contact deformation of the plate and the impactor as well as bending, transverse shear, and membrane deformations of the plate. The plate was transversely isotropic graphite/epoxy composite laminate and the impactor was a steel sphere. Calculated impact forces from the two analyses agreed with each other. The analyses were verified by comparing the results with reported test data.
Document ID
19840003151
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Shivakumar, K. N.
(NASA Langley Research Center Hampton, VA, United States)
Elber, W.
(NASA Langley Research Center Hampton, VA, United States)
Illg, W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1983
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:85703
NASA-TM-85703
Report Number: NAS 1.15:85703
Report Number: NASA-TM-85703
Accession Number
84N11219
Funding Number(s)
PROJECT: RTOP 506-53-23-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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