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Survivability characteristics of composite compression structureTest and evaluation was performed to determine the compression residual capability of graphite reinforced composite panels following perforation by high-velocity fragments representative of combat threats. Assessments were made of the size of the ballistic damage, the effect of applied compression load at impact, damage growth during cyclic loading and residual static strength. Several fiber/matrix systems were investigated including high-strain fibers, tough epoxies, and APC-2 thermoplastic. Additionally, several laminate configurations were evaluated including hard and soft laminates and the incorporation of buffer strips and stitching for improved damage resistance of tolerance. Both panels (12 x 20-inches) and full scale box-beam components were tested to assure scalability of results. The evaluation generally showed small differences in the responses of the material systems tested. The soft laminate configurations with concentrated reinforcement exhibited the highest residual strength. Ballistic damage did not grow or increase in severity as a result of cyclic loading, and the effects of applied load at impact were not significant under the conditions tested.
Document ID
19920023334
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Avery, John G.
(Boeing Military Airplane Development Wichita, KS, United States)
Allen, M. R.
(Boeing Military Airplane Development Wichita, KS, United States)
Sawdy, D.
(Boeing Military Airplane Development Wichita, KS, United States)
Avery, S.
(Wichita State Univ. KS., United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1990
Publication Information
Publication: NASA. Langley Research Center, Eighth DOD(NASA)FAA Conference on Fibrous Composites in Structural Design, Part 2
Subject Category
Composite Materials
Accession Number
92N32578
Funding Number(s)
CONTRACT_GRANT: F33615-83-C-3228
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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