| 000 | 01182nam a2200241Ia 4500 | ||
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| 003 | MX-MdCICY | ||
| 005 | 20250625124703.0 | ||
| 040 | _cCICY | ||
| 090 | _aB-7550 | ||
| 245 | 1 | 0 | _aMicromechanics of reinforcement and damage initiation in carbon fibre/epoxy composites under fatigue loading |
| 490 | 0 | _vComposites: Part A, 32A(3-4), p.457-471, 2001 | |
| 520 | 3 | _aA model single carbon fibre/epoxy composite geometry was subjected to cyclic loading at a maximum strain below the critical fatigue limit of the matrix material. The carbon fibres were pre-strained prior to incorporation in the resin to ensure that they were free of thermally induced compression stresses in the axial direction. A strain controlled cyclic experiment from 0 to 0.5 | |
| 650 | 1 | 4 | _aFATIGUE |
| 650 | 1 | 4 | _aCARBON FIBRE |
| 650 | 1 | 4 | _aEPOXY RESIN |
| 650 | 1 | 4 | _aINTERFACE |
| 700 | 1 | 2 | _aKoimtzoglou, C. |
| 700 | 1 | 2 | _aKostopoulos, V. |
| 700 | 1 | 2 | _aGaliotis, C. |
| 856 | 4 | 0 |
_uhttps://drive.google.com/file/d/1O8Xblb00-Mwt2kRqcRdRW_E4eVv8Q0aN/view?usp=drivesdk _zPara ver el documento ingresa a Google con tu cuenta: @cicy.edu.mx |
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