scholarly journals VOID GROWTH DURING HIGH VELOCITY IMPACT : EXPERIMENT AND MODEL

1991 ◽  
Vol 01 (C3) ◽  
pp. C3-605-C3-612 ◽  
Author(s):  
M. J. WORSWICK ◽  
B. WONG ◽  
R. J. PICK
Keyword(s):  
Void Growth ◽  
High Velocity ◽  
High Velocity Impact ◽  
Velocity Impact ◽  
Impact Experiment

High‐velocity impact experiment of concrete panels reinforced with crimped wire mesh and steel fibers

2018 ◽  
Vol 19 (6) ◽  
pp. 1818-1828 ◽  
Author(s):  
Sanghee Kim ◽  
Thomas H.‐K. Kang ◽  
Seok Joon Jang ◽  
Kang Su Kim ◽  
Hyun Do Yun
Keyword(s):  
High Velocity ◽  
Steel Fibers ◽  
Wire Mesh ◽  
High Velocity Impact ◽  
Velocity Impact ◽  
Concrete Panels ◽  
Impact Experiment

scholarly journals High velocity impact experiment (HVIE)

1998 ◽  
Author(s):  
A. Toor ◽  
T. Donich ◽  
P. Carter
Keyword(s):  
High Velocity ◽  
High Velocity Impact ◽  
Velocity Impact ◽  
Impact Experiment

High-velocity impact experiment of aluminum foam sample using powder gun

Measurement ◽  
2011 ◽  
Vol 44 (10) ◽  
pp. 2185-2189 ◽  
Author(s):  
Shigeru Tanaka ◽  
Kazuyuki Hokamoto ◽  
Seiichi Irie ◽  
Toshihiko Okano ◽  
Zoran Ren ◽  
...  
Keyword(s):  
High Velocity ◽  
Aluminum Foam ◽  
High Velocity Impact ◽  
Foam Sample ◽  
Velocity Impact ◽  
Impact Experiment

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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