| 000 | 01707nam a2200229Ia 4500 | ||
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| 003 | MX-MdCICY | ||
| 005 | 20250625124638.0 | ||
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| 090 | _aB-6208 | ||
| 245 | 1 | 0 | _aOnset of matrix cracking in angle-ply ceramic matrix composites |
| 490 | 0 | _vInternational Journal of Mechanical Sciences, 44(10), p.2173-2187 , 2002 | |
| 520 | 3 | _aThe problem of initial damage in angle-ply [-m/0n/m]and [-/]ceramic matrix composites subjected to axial tension is considered in this paper. The damage is in the form of matrix cracks that may appear in either inclined (- and lamination angle)or longitudinal layers. As follows from the analysis, if the lamination angle of the inclined layers is small, the initial failure occurs in the 0-layers of [-m/0n/m]composites or in [-/]composites in the form of bridging cracks. However, if the inclined layers form a larger angle with the load direction, they fail due to tunneling cracks. It is shown that the boundary between two different modes of failure in a representative SiC/CAS composite corresponds to a lamination angle equal to 35° in the case of [-m/0n/m]composites. In the case of [-/]laminates, the boundary value of the lamination angle is equal to 45°, i.e. bridging cracks form if <45° and tunneling cracks appear if >45° | |
| 650 | 1 | 4 | _aCERAMIC MATRIX COMPOSITES |
| 650 | 1 | 4 | _aMATRIX CRACKS |
| 650 | 1 | 4 | _aRESIDUAL STRESSES |
| 650 | 1 | 4 | _aFRACTURE |
| 700 | 1 | 2 | _aByrd, L.W. |
| 700 | 1 | 2 | _aBirman, V. |
| 856 | 4 | 0 |
_uhttps://drive.google.com/file/d/1yuZo0UBZXDGZbB_W8SShK8wTjONfHYf7/view?usp=drivesdk _zPara ver el documento ingresa a Google con tu cuenta: @cicy.edu.mx |
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