TY - JOUR
T1 - Stress transfer in the fibre fragmentation test. Part III Effects of interface debonding and matrix yielding
AU - Kim, Jang Kyo
N1 - Funding Information:
The author wishes to thank the Research Grants Council (RGC) for the financial support of this work. Part of the paper has been presented at the 10th International Conference in Composite Materials (ICCM-10), Whistler, Canada, August 1995.
PY - 1997
Y1 - 1997
N2 - The micromechanics of stress transfer is presented for the fibre fragmentation test of microcomposites containing debonded fibre matrix interface and yielded matrix at the interface region. Results from the parametric study are discussed for carbon fibre composites containing epoxy and polyetheretherketone (PEEK) matrices, representing respectively typical brittle debonding and matrix yielding behaviour at the interface region. The stress transfer phenomena are characterized for the two interface failure processes. The sequence of interface failure and fibre fracture as a function of applied stress are also identified. Maximum debonded and yielded interface lengths are obtained above which a fibre will fracture into smaller lengths. There are also threshold fibre fragment lengths above which fibre will fracture without interface debonding or matrix yielding. The applied stresses for these conditions are governed by three strength properties of the composite constituents, namely interface shear bond strength, matrix shear yield strength and fibre tensile strength forgiven elastic constants of the fibre and matrix, and the geometric factors of the microcomposite. The ineffective length, a measure of the efficiency of stress transfer across the fibre matrix interface, is shown to strongly depend on the extent to which these failure mechanisms take place at the interface region.
AB - The micromechanics of stress transfer is presented for the fibre fragmentation test of microcomposites containing debonded fibre matrix interface and yielded matrix at the interface region. Results from the parametric study are discussed for carbon fibre composites containing epoxy and polyetheretherketone (PEEK) matrices, representing respectively typical brittle debonding and matrix yielding behaviour at the interface region. The stress transfer phenomena are characterized for the two interface failure processes. The sequence of interface failure and fibre fracture as a function of applied stress are also identified. Maximum debonded and yielded interface lengths are obtained above which a fibre will fracture into smaller lengths. There are also threshold fibre fragment lengths above which fibre will fracture without interface debonding or matrix yielding. The applied stresses for these conditions are governed by three strength properties of the composite constituents, namely interface shear bond strength, matrix shear yield strength and fibre tensile strength forgiven elastic constants of the fibre and matrix, and the geometric factors of the microcomposite. The ineffective length, a measure of the efficiency of stress transfer across the fibre matrix interface, is shown to strongly depend on the extent to which these failure mechanisms take place at the interface region.
UR - http://www.scopus.com/inward/record.url?scp=0031079476&partnerID=8YFLogxK
U2 - 10.1023/A:1018596004325
DO - 10.1023/A:1018596004325
M3 - Article
AN - SCOPUS:0031079476
SN - 0022-2461
VL - 32
SP - 701
EP - 711
JO - Journal of Materials Science
JF - Journal of Materials Science
IS - 3
ER -