3D Computer Modeling of High-Velocity Impact Phenomena

2006 ◽  
Author(s):  
V. V. Kim
Keyword(s):  
Computer Modeling ◽  
High Velocity ◽  
High Velocity Impact ◽  
Velocity Impact ◽  
Impact Phenomena

Models of high velocity impact phenomena

1993 ◽  
Vol 14 (1-4) ◽  
pp. 819-830 ◽  
Author(s):  
C.A. Wingate ◽  
R.F. Stellingwerf ◽  
R.F. Davidson ◽  
M.W. Burkett
Keyword(s):  
High Velocity ◽  
High Velocity Impact ◽  
Velocity Impact ◽  
Impact Phenomena

Computer modeling of the dynamics of high-velocity impact and accompanying physical phenomena

1992 ◽  
Vol 35 (8) ◽  
pp. 690-723 ◽  
Author(s):  
N. N. Belov ◽  
V. N. Demidov ◽  
L. V. Efremova ◽  
A. V. Zhukov ◽  
A. P. Nikolaev ◽  
...  
Keyword(s):  
Computer Modeling ◽  
High Velocity ◽  
High Velocity Impact ◽  
Velocity Impact ◽  
Physical Phenomena

Effect of strain rate, off-axis loading and high-velocity impact damage on the compressive strength of C/SiC composite

2018 ◽  
Vol 53 (4) ◽  
pp. 535-546 ◽  
Author(s):  
M Altaf ◽  
S Singh ◽  
VV Bhanu Prasad ◽  
Manish Patel
Keyword(s):  
Compressive Strength ◽  
Strain Rate ◽  
High Velocity ◽  
Impact Damage ◽  
The Other ◽  
High Velocity Impact ◽  
Fibre Bundles ◽  
Velocity Impact ◽  
Kink Bands ◽  
Other Hand

The compressive strength of C/SiC composite at different strain rates, off-axis orientations and after high-velocity impact was studied. The compressive strength was found to be 137 ± 23, 130 ± 46 and 162 ± 33 MPa at a strain rate of 3.3 × 10−5, 3.3 × 10−3, 3.3 × 10−3 s−1, respectively. On the other hand, the compressive strength was found to be 130 ± 46, 99 ± 23 and 87 ± 9 MPa for 0°/90°, 30°/60° and 45°/45° fibre orientations to loading direction, respectively. After high-velocity impact, the residual compressive strength of C/SiC composite was found to be 58 ± 26, 44 ± 18 and 36 ± 3.5 MPa after impact with 100, 150 and 190 m/s, respectively. The formation of kink bands in fibre bundles was found to be dominant micro-mechanism for compressive failure of C/SiC composite for 0°/90° orientation. On the other hand, delamination and the fibre bundles rotation were found to be the dominant mechanism for off-axis failure of composite.

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