TY - GEN
T1 - Impact compressive character of balanced angle-ply carbon/epoxy cmposites
AU - Tian, Chun Lei
AU - Pi, Ai Guo
AU - Huang, Feng Lei
PY - 2011
Y1 - 2011
N2 - This paper discusses the response of balanced angle-ply graphite/epoxy composite laminates subjected to different strain rate compression loading using a compression split Hopkinson's pressure bar (SHPB) and an MTS machine. Five types of laminates, with ply angles 0°, ±15°, ±45°, ±75° and 90°were manufactured using T700 carbon fiber with epoxy resin system by hand. Samples were subjected to compression loading at different strain rates along longitudinal direction. The stress-strain curves at different strain rates were compared for each sample type. Characteristics of the curves were summarized and the causes were analyzed. Finally, the relationship between failure strength and ply angles was analyzed.
AB - This paper discusses the response of balanced angle-ply graphite/epoxy composite laminates subjected to different strain rate compression loading using a compression split Hopkinson's pressure bar (SHPB) and an MTS machine. Five types of laminates, with ply angles 0°, ±15°, ±45°, ±75° and 90°were manufactured using T700 carbon fiber with epoxy resin system by hand. Samples were subjected to compression loading at different strain rates along longitudinal direction. The stress-strain curves at different strain rates were compared for each sample type. Characteristics of the curves were summarized and the causes were analyzed. Finally, the relationship between failure strength and ply angles was analyzed.
KW - Carbon/epoxy composite
KW - Composite
KW - Hopkinson's pressure bar
KW - Strain rate
UR - http://www.scopus.com/inward/record.url?scp=79960760136&partnerID=8YFLogxK
U2 - 10.4028/www.scientific.net/AMR.284-286.132
DO - 10.4028/www.scientific.net/AMR.284-286.132
M3 - Conference contribution
AN - SCOPUS:79960760136
SN - 9783037851913
T3 - Advanced Materials Research
SP - 132
EP - 135
BT - Materials and Design
T2 - 2011 International Conference on Advanced Engineering Materials and Technology, AEMT 2011
Y2 - 29 July 2011 through 31 July 2011
ER -