Microstructure Inhomogeneities in 2519A Aluminum Plate Penetrated by an Incendiary Projectile

2007 ◽  
Vol 546-549 ◽  
pp. 1049-1054 ◽  
Author(s):  
Hui Gao ◽  
Xin Ming Zhang ◽  
Hui Zhong Li ◽  
Ying Liu

2519A aluminum plate was shot obliquely by an incendiary projectile with the diameter of 7.62mm at impact velocity of 818m/s. The penetration inhomogeneities of the crater of 2519A aluminum target plate were investigated with optical microscopy (OM), scanning electron microscopy (SEM). Melted substance, a mixture of the target material and the projectile was found at the interface of target and projectile. Different microstructural characteristics were observed along the crater depth. Grains were elongated near the entrance area, while severely kinked grains and adiabatic shear bands were present in the middle region, and microbands, as well as abnormal grown grains, appeared at the crater bottom. The failure form of target is mainly ductile expanding.

2021 ◽  
Vol 1035 ◽  
pp. 39-45
Author(s):  
Jing Li ◽  
Zhi Shou Zhu ◽  
Xin Nan Wang ◽  
Tao Jiang

The penetration damaging behavior of ATI425 titanium alloy was studied by 7.62 mm diameter armor piercing projectiles. The damage characteristics and the mechanism were analyzed by observing and analyzing the craters of ATI425 titanium alloy target. It can be found that local temperature-rise of the target plate occurred, even sputtering phenomenon in the opening stage. The shear bands extended upward along the cater wall could be seen in the stable stage. The large non-homogeneous deformation in adiabatic shear bands caused microcracks and micropores. A large number of macro-cracks were observed on the side wall and at the bottom of the crater.


2013 ◽  
Vol 58 (4) ◽  
pp. 1207-1212
Author(s):  
E.S. Dzidowski

Abstract The causes of plane crashes, stemming from the subcritical growth of fatigue cracks, are examined. It is found that the crashes occurred mainly because of the negligence of the defects arising in the course of secondary metalworking processes. It is shown that it is possible to prevent such damage, i.e. voids, wedge cracks, grain boundary cracks, adiabatic shear bands and flow localization, through the use of processing maps indicating the ranges in which the above defects arise and the ranges in which safe deformation mechanisms, such as deformation in dynamic recrystallization conditions, superplasticity, globularization and dynamic recovery, occur. Thanks to the use of such maps the processes can be optimized by selecting proper deformation rates and forming temperatures.


2021 ◽  
Vol 1121 (1) ◽  
pp. 012007
Author(s):  
I Mania ◽  
H Paul ◽  
R Chulist ◽  
P Petrzak

1999 ◽  
Vol 42 (1) ◽  
pp. 61-71 ◽  
Author(s):  
A.V Dobromyslov ◽  
N.I Taluts ◽  
N.V Kazantseva ◽  
E.A Kozlov

2007 ◽  
Vol 457 (1-2) ◽  
pp. 205-218 ◽  
Author(s):  
J.F.C. Lins ◽  
H.R.Z. Sandim ◽  
H.-J. Kestenbach ◽  
D. Raabe ◽  
K.S. Vecchio

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