TY - JOUR
T1 - Mechanical and chemical consequences of through thickness thermal gradients in polyimide matrix composite materials
AU - Drukker, E.
AU - Green, A. K.
AU - Marom, G.
PY - 2003/2
Y1 - 2003/2
N2 - Composite material parts may be exposed during their service life to through thickness temperature gradients where the difference between the inner and outer faces may exceed 150°C. The effect of these conditions on 4,4′-bismaleimidodiphenylmethane and diallylbisphenol-A based BMI resin reinforced with glass fabrics was investigated as a function of location through the laminate thickness. It was found that a gradient of chemical, physical and mechanical properties exists through the laminate thickness. A decrease of interlaminar shear strength and an increase of glass transition temperature follow high temperature exposure that causes resin chemistry changes. The material becomes less flexible and more sensitive to microcrack development as a result of these changes.
AB - Composite material parts may be exposed during their service life to through thickness temperature gradients where the difference between the inner and outer faces may exceed 150°C. The effect of these conditions on 4,4′-bismaleimidodiphenylmethane and diallylbisphenol-A based BMI resin reinforced with glass fabrics was investigated as a function of location through the laminate thickness. It was found that a gradient of chemical, physical and mechanical properties exists through the laminate thickness. A decrease of interlaminar shear strength and an increase of glass transition temperature follow high temperature exposure that causes resin chemistry changes. The material becomes less flexible and more sensitive to microcrack development as a result of these changes.
KW - B. Environmental degradation
KW - B. High-temperature properties
KW - E. Resin transfer moulding(RTM)
KW - Temperature gradient
UR - http://www.scopus.com/inward/record.url?scp=0037330476&partnerID=8YFLogxK
U2 - 10.1016/S1359-835X(02)00261-0
DO - 10.1016/S1359-835X(02)00261-0
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AN - SCOPUS:0037330476
SN - 1359-835X
VL - 34
SP - 125
EP - 133
JO - Composites Part A: Applied Science and Manufacturing
JF - Composites Part A: Applied Science and Manufacturing
IS - 2
ER -