TY - JOUR
T1 - Failure Characteristics of 6061/Al2O3/15p and 2014/Al2O3/15p Composites as a Function of Loading Rate
AU - LOU, B.Y.
AU - HUANG, J.C.
PY - 1996/10
Y1 - 1996/10
N2 - The effects of loading rate on the toughness and fracture mechanisms of two cast 6061/Al2O3/15p and 2014/Al2O3/15p composites under the as-worked (AW) and AW + T6 conditions have been examined. The quasistatic bending and high-rate impact tests were conducted over strain rates from 5 × 10-4 to 1 × 103 s-1 using screw-driven or servohydraulic high-rate systems. The results showed that the peak load Pmax, specimen deflection d, specimen lateral expansion fraction Δw, crack initiation energy Ei, propagation energy Ep, total fracture energy Et, and deformation zone all tended to increase with increasing strain rate. Under quasistatic loading, the composites failed predominantly by matrix/reinforcement interface decohesion. As the loading rate increased, reinforcement failure became the major failure mechanism. Differences in the effect of matrix microstructure and stress state on the fracture properties also are discussed. In comparing the fracture modes in the AW and AW + T6 specimens, the latter showed a higher tendency toward particle cracking. Based on mechanical data, the degree of specimen deflection and expansion and fracture modes, the AW composites exhibited a higher strain-rate dependence. The T6 specimens, due to their intrinsicly more brittle nature, appeared to be less influenced by loading rate over the strain-rate range examined.
AB - The effects of loading rate on the toughness and fracture mechanisms of two cast 6061/Al2O3/15p and 2014/Al2O3/15p composites under the as-worked (AW) and AW + T6 conditions have been examined. The quasistatic bending and high-rate impact tests were conducted over strain rates from 5 × 10-4 to 1 × 103 s-1 using screw-driven or servohydraulic high-rate systems. The results showed that the peak load Pmax, specimen deflection d, specimen lateral expansion fraction Δw, crack initiation energy Ei, propagation energy Ep, total fracture energy Et, and deformation zone all tended to increase with increasing strain rate. Under quasistatic loading, the composites failed predominantly by matrix/reinforcement interface decohesion. As the loading rate increased, reinforcement failure became the major failure mechanism. Differences in the effect of matrix microstructure and stress state on the fracture properties also are discussed. In comparing the fracture modes in the AW and AW + T6 specimens, the latter showed a higher tendency toward particle cracking. Based on mechanical data, the degree of specimen deflection and expansion and fracture modes, the AW composites exhibited a higher strain-rate dependence. The T6 specimens, due to their intrinsicly more brittle nature, appeared to be less influenced by loading rate over the strain-rate range examined.
KW - Material Transaction
KW - Composite Specimen
KW - Increase Strain Rate
KW - Major Crack
KW - Ductility Index
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U2 - 10.1007/bf02663859
DO - 10.1007/bf02663859
M3 - RGC 21 - Publication in refereed journal
SN - 1073-5623
VL - 27
SP - 3095
EP - 3107
JO - Metallurgical and Materials Transactions A: Physical Metallurgy and Materials Science
JF - Metallurgical and Materials Transactions A: Physical Metallurgy and Materials Science
IS - 10
ER -