Thermomechanical assessment of damage in composites
暂无分享,去创建一个
[1] R. D. Henshell,et al. CRACK TIP FINITE ELEMENTS ARE UNNECESSARY , 1975 .
[2] T. O'Brien. Characterization of delamination onset and growth in a composite laminate , 1982 .
[3] Jehuda Tirosh,et al. A semi-automated in-plane loader for materials testing , 1983 .
[4] Alan Baker,et al. Repair of mirage III aircraft using the BFRP crack-patching technique , 1984 .
[5] J. Comyn,et al. Structural Adhesive Joints in Engineering , 1984, The Aeronautical Journal (1968).
[6] A. Baker,et al. Damage tolerance of graphite/epoxy composites , 1985 .
[7] A. Machin,et al. Mean stress dependence of the thermoelastic constant , 1987 .
[8] R. Jones,et al. Thermoelastic constant or thermoelastic parameter , 1987 .
[9] J. F. Williams,et al. Assessment of the effect of impact damage in composites: Some problems and answers , 1988 .
[10] L. Molent,et al. Bonded repair of metallic components: Thick sections , 1988 .
[11] A. K. Wong,et al. On the revised theory of the thermoelastic effect , 1988 .
[12] D. Saunders,et al. Effect of load duration on the fatigue behaviour of graphite/epoxy laminates containing delaminations , 1988 .
[13] J. F. Williams,et al. Thermomechanical behaviour of composites , 1989 .