TY - JOUR
T1 - Radial matrix cracking and interphase failure in transversely loaded fiber composites
AU - Zhu, H.
AU - Achenbach, J. D.
N1 - Funding Information:
This work was carried out in the course of research sponsored by the Air Force Office of Scientific Research under Grant AFOSR-88-0124. The authors would like to acknowledge helpful discussions with Professor I.M. Daniel and George Anastassopoulos.
PY - 1991/7
Y1 - 1991/7
N2 - Radial matrix cracking and interphase failure for transverse loading of a hexagonal array fiber composite are investigated by: (1) modeling the interphase by a layer of radial and circumferential spring elements, (2) adopting a tensile stress criterion for initiation of matrix cracking, and (3) employing a strain-energy density criterion for interphase failure. The mechanical behavior of the composite is defined in terms of geometrical, stiffness and strength parameters. Stresses on the microlevel have been calculated. Under the assumption that the failure mechanisms follow the periodicity of the composite, two scenarios related to different values of the strength parameters have been investigated. In the first scenario matrix cracking occurs first, followed by interphase failure. In the second scenario interphase failure is followed by matrix cracking. Typical results are displayed graphically.
AB - Radial matrix cracking and interphase failure for transverse loading of a hexagonal array fiber composite are investigated by: (1) modeling the interphase by a layer of radial and circumferential spring elements, (2) adopting a tensile stress criterion for initiation of matrix cracking, and (3) employing a strain-energy density criterion for interphase failure. The mechanical behavior of the composite is defined in terms of geometrical, stiffness and strength parameters. Stresses on the microlevel have been calculated. Under the assumption that the failure mechanisms follow the periodicity of the composite, two scenarios related to different values of the strength parameters have been investigated. In the first scenario matrix cracking occurs first, followed by interphase failure. In the second scenario interphase failure is followed by matrix cracking. Typical results are displayed graphically.
UR - http://www.scopus.com/inward/record.url?scp=0026187729&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0026187729&partnerID=8YFLogxK
U2 - 10.1016/0167-6636(91)90032-U
DO - 10.1016/0167-6636(91)90032-U
M3 - Article
AN - SCOPUS:0026187729
SN - 0167-6636
VL - 11
SP - 347
EP - 356
JO - Mechanics of Materials
JF - Mechanics of Materials
IS - 4
ER -