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Energy absorption of composite materialsResults of a study on the energy absorption characteristics of selected composite material systems are presented and the results compared with aluminum. Composite compression tube specimens were fabricated with both tape and woven fabric prepreg using graphite/epoxy (Gr/E), Kevlar (TM)/epoxy (K/E) and glass/epoxy (Gl/E). Chamfering and notching one end of the composite tube specimen reduced the peak load at initial failure without altering the sustained crushing load, and prevented catastrophic failure. Static compression and vertical impact tests were performed on 128 tubes. The results varied significantly as a function of material type and ply orientation. In general, the Gr/E tubes absorbed more energy than the Gl/E or K/E tubes for the same ply orientation. The 0/ + or - 15 Gr/E tubes absorbed more energy than the aluminum tubes. Gr/E and Gl/E tubes failed in a brittle mode and had negligible post crushing integrity, whereas the K/E tubes failed in an accordian buckling mode similar to the aluminum tubes. The energy absorption and post crushing integrity of hybrid composite tubes were not significantly better than that of the single material tubes.
Document ID
19830011545
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Farley, G. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1983
Subject Category
Composite Materials
Report/Patent Number
AVRADCOM-TR-83-B-2
NASA-TM-84638
NAS 1.15:84638
Report Number: AVRADCOM-TR-83-B-2
Report Number: NASA-TM-84638
Report Number: NAS 1.15:84638
Meeting Information
Meeting: Natl. Specialists'' Meeting: Composite Structures
Start Date: March 1, 1983
Sponsors: American Helicopter Society
Accession Number
83N19816
Funding Number(s)
PROJECT: RTOP 505-42-23-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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