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Tensile behavior of C/SiC composites plate after hypervelocity penetration: Residual strength and fracture mechanism
- Source :
- Composite Structures. 189:378-385
- Publication Year :
- 2018
- Publisher :
- Elsevier BV, 2018.
-
Abstract
- The damage and tensile mechanical behavior of C/SiC composites plate after hypervelocity penetration are studied in this paper. Hypervelocity penetration is applied along the out-of-plane direction by an electrical gun at 3.5 km s - 1 , and the target is recovered for damage observation and tension test. Quasi-static tensions on the recovered targets and the slices cut from damage zone are examined along with high-speed photography. Moreover, corresponding numerical simulations are carried out. The damage zone in the vicinity of the penetration hole is small ( ∼ 10 mm), and the damage mode involves SiC matrix fracture, delamination, fiber bundle splitting and fiber breaking. The simulation results suggest that the degree of damage decreases exponentially with the increasing distance from the penetration hole center of the target plate. As the degree of damage increases, the tensile strength of C/SiC composites decreases and the corresponding fracture mode changes from shear failure to tensile breakage. Additionally the fracture surface becomes smoother, the quantity and length of fiber pullout also increases. Since the decrease of elastic modulus induced by damage weakens the stress concentration effect of the penetration hole, the residual strength of recovered target plate is only reduced from 241 MPa to 175 MPa.
- Subjects :
- Materials science
02 engineering and technology
Penetration (firestop)
021001 nanoscience & nanotechnology
Residual strength
020303 mechanical engineering & transports
0203 mechanical engineering
Breakage
Ultimate tensile strength
Ceramics and Composites
Hypervelocity
Composite material
0210 nano-technology
Elastic modulus
Civil and Structural Engineering
Stress concentration
Tensile testing
Subjects
Details
- ISSN :
- 02638223
- Volume :
- 189
- Database :
- OpenAIRE
- Journal :
- Composite Structures
- Accession number :
- edsair.doi...........3993d895a4325e07038dcaa6d534b6f3
- Full Text :
- https://doi.org/10.1016/j.compstruct.2018.01.058