𝔖 Bobbio Scriptorium
✦   LIBER   ✦

On the cyclic crack-tip opening displacement

✍ Scribed by A. J. McEVILY

Book ID
109015467
Publisher
John Wiley and Sons
Year
2009
Tongue
English
Weight
112 KB
Volume
32
Category
Article
ISSN
8756-758X

No coin nor oath required. For personal study only.

πŸ“œ SIMILAR VOLUMES

The effect of shallow cracks on crack ti
The effect of shallow cracks on crack tip opening displacement
✍ G. Matsoukas; B. Cotterell; Y.-W. Mai πŸ“‚ Article πŸ“… 1986 πŸ› Elsevier Science 🌐 English βš– 441 KB

Further resuhs given in the present paper confnm that shallow cracks have larger crack tip opening disp~a~en~ at initiation than deep cracks. This difference in behaviour is shown to be principally caused by the different hydrostatic stresses existing at the tips of shallow and deep cracks. A new me

Critical crack tip opening displacement
Critical crack tip opening displacement for polymer composites
✍ C. Vipulanandan; N. Dharmarajan πŸ“‚ Article πŸ“… 1989 πŸ› Elsevier Science 🌐 English βš– 1017 KB

Applicability of critical stress intensity factor (K,) and/or critical crack tip opening displacement (CTODA for epoxy and polyester polymer composites (PC) in mode I fracture are investigated. Both unreinforced and glass fiber reinforced polymer composite systems are studied using single edge notch

On the influence of specimen geometry on
On the influence of specimen geometry on the critical crack-tip-opening displacement
✍ O. Kolednik; P. KutlesΜ†a πŸ“‚ Article πŸ“… 1989 πŸ› Elsevier Science 🌐 English βš– 822 KB

Critical values of the crack-tip-opening displacement, COD,, are determined on CIIspecimens having different thicknesses and ligament lengths. COD, is determined using the method of stereophotogrammetry with the scanning-electron microscope. The in&nce of specimen geometry on CODi is studied. Criter

Prediction of crack tip opening displace
Prediction of crack tip opening displacement of fibre composites
✍ V.K Srivastava πŸ“‚ Article πŸ“… 1992 πŸ› Elsevier Science 🌐 English βš– 293 KB

The fracture behaviour of single edge notched unidirectional glass fibre reinforced epoxy resin composites under tensile loading was investigated. Loadelongation curves were obtained for crack length varying from 4, 6, 8, 10 and 12mm and different fibre volume fractions of 0.48, 0.502 and 0.525. The