NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Influence of Fiber Volume and Alignment on Impact Resistance of Braided Carbon Fiber Epoxy CompositesThe effect of axial tow alignment within a laminate ply stack on the impact penetration threshold for a series of composite panels was evaluated; specifically, the effect of a lateral shift in alignment to induce fiber nesting. Panels were fabricated from braided T700S carbon fiber and TenCate Advanced Composites's TC275-1 epoxy resin prepreg. Axial tows in each ply were aligned, offset, or rotated to evaluate the influence of such parameters on impact penetration resistance. Panel-to-panel variation in thickness, resin content, and fiber volume ratio were measured. Ultimately, process-related deviations drove penetration limits on impact. Influence of axial tow alignment was difficult to discern outside of the processing-induced variations between panels.
Document ID
20180004929
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Miller, Sandi G.
(NASA Glenn Research Center Cleveland, OH, United States)
Roberts, Gary D.
(NASA Glenn Research Center Cleveland, OH, United States)
Heimann, Paula J.
(Ohio Aerospace Inst. Brook Park, OH, United States)
McCorkle, Linda S.
(Ohio Aerospace Inst. Brook Park, OH, United States)
Martin, Richard E.
(Cleveland State Univ. Cleveland, OH, United States)
Pereira, J. Michael
(NASA Glenn Research Center Cleveland, OH, United States)
Goldberg, Robert K.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2018
Publication Date
July 1, 2018
Subject Category
Composite Materials
Report/Patent Number
NASA/TM-2018-219881
GRC-E-DAA-TN53689
E-19504
Funding Number(s)
WBS: WBS 826611.04.03.01
CONTRACT_GRANT: NNC13BA10B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
process variation
ballistic impact
epoxy
No Preview Available