Local field effects in titanium matrix composites subject to fiber-matrix debonding

International Journal of Plasticity

Volumn 20, Issue 8-9, 2004, Pages 1707-1737

  Bednarcyk, Brett A ^a   Arnold, Steven M ^b   Aboudi, Jacob ^c   Pindera, Marek Jerzy ^a  

^a UNIVERSITY OF VIRGINIA   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

^c TEL AVIV UNIVERSITY   (Israel)

Author keywords

High fidelity generalized method of cells (HFGMC); Interfacial debonding; Metal matrix composites; Micromechanics; Viscoplasticity

Indexed keywords

COMPOSITE MICROMECHANICS; DEBONDING; DEFORMATION; INTERFACES (MATERIALS); MATHEMATICAL MODELS; VISCOPLASTICITY;

HIGH FIDELITY GENERALIZED METHOD OF CELLS (HFGMC); INTERFACIAL DEBONDING; LOCAL FIELD EFFECTS;

METALLIC MATRIX COMPOSITES;

EID: 2342486012     PISSN: 07496419     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijplas.2003.11.019     Document Type: Article

References (40)

1. Aboudi J. Damage in composites - modeling of imperfect bonding. Composites Science and Technology. 28:1987;103-128.
2. Aboudi J., Pindera M.-J., Arnold S.M. Linear thermoelastic higher-order theory for periodic multiphase materials. Journal of Applied Mechanics. 68:2001;697-707.
3. Aboudi J., Pindera M.-J., Arnold S.M. Higher-order theory for periodic multiphase materials with inelastic phases. International Journal of Plasticity. 19:2003;805-847. See also NASA/TM-2002-211469.
4. Achenbach J.D., Zhu H. Effect of interfacial zone on mechanical behavior and failure of fiber-reinforced composites. Journal of the Mechanics and Physics of Solids. 37:1989;381-393.
5. Arnold, S.M., Saleeb, A.F., Castelli, M.G., 1994. A fully associative, nonisothermal, nonlinear kinematic, unified viscoplastic model for titanium alloys. NASA TM 106926.
6. Bansal, Y., Pindera, M.-J., 2002. Efficient reformulation of the thermoelastic higher order theory for FGMs. NASA/CR-2002-211909.
7. Baxter S.C., Hossain M.I., Graham L.L. Micromechanics based random material property fields for particulate reinforced composites. International Journal of Solids and Structures. 38:2001;9209-9220.
8. Bednarcyk, B.A., Arnold, S.M., 2000. A new local debonding model with application to the transverse tensile and creep behavior of continuously reinforced titanium composites. NASA/TM-2000-210029.
9. Bednarcyk B.A., Arnold S.M. Micromechanics-based deformation and failure prediction for longitudinally reinforced titanium composites. Composites Science and Technology. 61:2001;705-729.
10. Bednarcyk B.A., Arnold S.M. Transverse tensile and creep modeling of continuously reinforced titanium composites with local debonding. International Journal of Solids and Structures. 39:2002;1987-2017.
11. Bonfoh N., Lipinski P., Carmasol A., Tiem S. Micromechanical modeling of ductile damage of polycrystalline materials with heterogeneous particles. International Journal of Plasticity. 20:2004;85-106.
12. Cervay, R.R., 1994. SCS-6/β21S and SCS-9/β21S mechanical property evaluation. NASP CR-1165.
13. Chen J.K., Huang Z.P., Mai Y.W. Constitutive relation of particulate-reinforced viscoelastic composite materials with debonded microvoids. Acta Materialia. 51:2003;3375-3384.
14. Eggleston, M.R., 1993. Testing, modeling, and analysis of transverse creep in SCS-6/Ti-6Al-4V metal matrix composites at 482 °C. GE Research and Development Center Report 93CRD163.
15. Ellyin F., Xia Z. Rate-dependent constitutive modelling and micro-mechanical analysis of fibre-reinforced metal-matrix composites. Journal of the Mechanics and Physics of Solids. 49:2001;2543-2555.
16. Goda K. Creep-rupture lifetime simulation of unidirectional metal matrix composites with and without time-dependent fiber breakage. International Journal of Plasticity. 18:2002;1729-1748.
17. Goldberg, R.K., Arnold, S.M., 2000. A study of influencing factors on the tensile response of a titanium matrix composite with weak interfacial bonding. NASA/TM-2000-209798.
18. Graham L.L., Baxter S.C. Simulation of local material properties based on moving-window GMC. Journal of Probabilistic Mechanics. 16:2001;295-305.
19. Gundel D.B., Warrier S.G., Miracle D.B. The transverse tensile behavior of SiC-fiber/Ti-6Al-4V composites 2. Stress distribution and interface failure. Composites Science and Technology. 59:1999;1087-1096.
20. 6/Ti-15-3 metal matrix composites at room temperature. Kennedy J.M., Moeller H.H., Johnson W.S. Thermal and Mechanical Behavior of Metal Matrix and Ceramic Matrix Composites, ASTM STP1080. 1990;193-218 American Society for Testing and Materials, Philadelphia.
21. Jones J.P., Whittier J.S. Waves at flexibly bonded interfaces. Journal of Applied Mechanics. 34:1967;905-909.
22. Lerch B.A., Saltzman J.F. Tensile deformation of SiC/Ti-15-3 laminates. Stinchcomb W.W., Ashbaugh N.E. Composite Materials: Fatigue and Fracture B, Fourth Volume, ASTM STP1156. 1993;161-175 American Society for Testing and Materials, Philadelphia.
23. Li Z., Guo W. The influence of plasticity mismatch on the growth and coalescence of spheroidal voids on the bimaterial interface. International Journal of Plasticity. 18:2002;249-279.
24. Lissenden C.J., Herakovich C.T. Interfacial debonding in titanium matrix composites. Mechanics of Materials. 22:1996;279-290.
25. Lissenden C.J., Herakovich C.T., Pindera M.-J. Inelastic Deformation of Titanium Matrix Composites Under Multiaxial Loading. Johnson W.S., Larson J.M., Cox B.N. Life Prediction Methodology for Titanium Matrix Composites, ASTM STP1253. 1996;257-277 American Society for Testing and Materials, Philadelphia.
26. Majumdar, B.S., Newaz, G.M., 1992. Inelastic deformation of metal matrix composites: plasticity and damage mechanisms. Philosophical Magazine A 66, 187-212 (see also NASA CR-189095).
27. McGee, J.D., Herakovich, C.T., 1992. Micromechanics of fiber/matrix debonding. Report AM-92-01, Applied Mechanics Program, University of Virginia, Charlottesville, Va.
28. Needleman A. A continuum model for void nucleation by inclusion debonding. Journal of Applied Mechanics. 54:1987;525-531.
29. Paley M., Aboudi J. Micromechanical analysis of composites by the generalized cells model. Mechanics of Materials. 14:1992;127-139.
30. Pindera M.-J., Bednarcyk B.A. An efficient implementation of the generalized method of cells for unidirectional, multi-phased composites with complex microstructures. Composites: Part B. 30:1999;87-105.
31. Robertson D.D., Mall S. Micromechanical analysis of metal matrix composite laminates with fiber/matrix interfacial debonding. Composites Engineering. 4:1994;1257-1274.
32. Saczuk J., Hackel K., Stumpf H. Rate theory of nonlocal gradient damage-gradient viscoinelasticity. International Journal of Plasticity. 19:2003;675-706.
33. Saleeb A.F., Arnold S.M., Castelli M.G., Wilt T.E., Graf W. A general hereditary multimechanism-based deformation model with application to the viscoelastoplastic response of titanium alloys. International Journal of Plasticity. 17:2001;1305-1350.
34. Sankurathri A., Baxter S., Pindera M.-J. The effect of fiber architecture on the inelastic response of metal matrix composites with interfacial and fiber damage. Voyiadjis G.Z., Allen D.H. Damage and Interfacial Debonding in Composites. 1996;235-257 Elsevier, New York.
35. Shabana Y.M. Incremental constitutive equation for discontinuously reinforced composites considering reinforcement damage and thermoelastoplasticity. Computational Materials Science. 28:2003;31-40.
36. Tvergaard V. Cohesive zone representation of failure between elastic or rigid solids and ductile solids. Engineering Fracture Mechanics. 70:2003;1859-1868.
37. Warrier S.G., Majumdar B.S., Miracle D.B. Determination of the interface failure mechanism during transverse loading of single fibre SiC/Ti-6Al-4V composites from torsion tests. Acta Materialia. 45:1997;309-320.
38. Warrier S.G., Majumdar B.S., Gundel D.B., Miracle D.B. Implications of tangential shear stress induced failure during transverse loading of SiC/Ti-6Al-4V composites. Acta Materialia. 45:1997;3469-3480.
39. Wilt, T.E., Arnold, S.M., 1996. Micromechanics analysis code (MAC) user guide: version 2.0. NASA TM 107290.
40. Zhong, Y., Pindera, M.-J., 2002. Efficient reformulation of HOTFGM: heat conduction with variable thermal conductivity. NASA/CR-2002-211910.