Numerical and experimental modeling of jet formation during a high-velocity oblique impact of metal plates

2012 ◽  
Vol 48 (2) ◽  
pp. 214-225 ◽  
Author(s):  
S. P. Kiselev ◽  
V. I. Mali
Keyword(s):  
High Velocity ◽  
Oblique Impact ◽  
Experimental Modeling ◽  
Jet Formation ◽  
Metal Plates

Wave formation in a high-velocity symmetric impact of metal plates

2006 ◽  
Vol 42 (5) ◽  
pp. 611-616 ◽  
Author(s):  
V. V. Pai ◽  
Ya. L. Luk’yanov ◽  
G. E. Kuz’min ◽  
I. V. Yakovlev
Keyword(s):  
High Velocity ◽  
Wave Formation ◽  
Metal Plates

scholarly journals Experimental investigation of high velocity oblique impact and residual tensile strength of carbon/epoxy laminates

2019 ◽  
Vol 182 ◽  
pp. 107772 ◽  
Author(s):  
Ashwin R. Kristnama ◽  
Xiaodong Xu ◽  
David Nowell ◽  
Michael R. Wisnom ◽  
Stephen R. Hallett
Keyword(s):  
Experimental Investigation ◽  
Tensile Strength ◽  
High Velocity ◽  
Oblique Impact

Plasticine modelled high velocity oblique impact and ricochet of long rods

1982 ◽  
Vol 24 (7) ◽  
pp. 437-455 ◽  
Author(s):  
W. Johnson ◽  
A.K. Sengupta ◽  
S.K. Ghosh
Keyword(s):  
High Velocity ◽  
Oblique Impact

Ballistic performance and damage simulation of fiber metal laminates under high-velocity oblique impact

2020 ◽  
Vol 29 (7) ◽  
pp. 1011-1034 ◽  
Author(s):  
Chao Zhang ◽  
Qian Zhu ◽  
Jose L Curiel-Sosa ◽  
Tinh Quoc Bui
Keyword(s):  
Impact Velocity ◽  
High Velocity ◽  
Damage Mechanics ◽  
Failure Modes ◽  
Element Model ◽  
Oblique Impact ◽  
Ballistic Performance ◽  
Fiber Metal Laminates ◽  
Fiber Metal ◽  
The Impact

Fiber metal laminates have been successfully applied in military aircrafts, armor vehicles and other modern engineering industries as protective structures due to their outstanding impact resistant properties. Prediction of the ballistic performance and investigation on the damage mechanism of the fiber metal laminates under general oblique impact conditions still remain a very challenging issue. In this study, a nonlinear dynamic finite element model in terms of continuum damage mechanics including intra- and inter-layer failure modes is presented. The accuracy of this model is validated with available experimental data. The damage and ballistic performance of two different structural fiber metal laminates subjected to high-velocity oblique impact by rigid hemispherical nose projectile with angles of 0°, 30°, 45° and 60° are studied. The numerical results show that the projectile deflects when the oblique impact occurs and the deflection angle decreases with increasing the impact velocity. The residual velocity of the projectile and the energy absorption of the target are related to the initial impact velocity and impact angle of the projectile. The proposed simulation approach offers a new proper reference for numerical investigations of common oblique impact problems in other fiber metal laminates.

The constitutive behavior of Ti–5Al–3V–2Cr–2Fe under high-velocity impact: Experimental, modeling, and validation

2019 ◽  
Vol 811 ◽  
pp. 151946 ◽  
Author(s):  
Ping Song ◽  
Wen-bin Li ◽  
Yu Zheng ◽  
Zhong-wei Guan ◽  
Xiao-ming Wang ◽  
...  
Keyword(s):  
High Velocity ◽  
Experimental Modeling ◽  
Constitutive Behavior ◽  
High Velocity Impact ◽  
Velocity Impact
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