Theoretical analysis of ionization of spherical aluminum alloy projectile impacting aluminum alloy target in hypervelocity impact

Author(s):  
Liangfei Gong ◽  
Qingming Zhang ◽  
Renrong Long ◽  
Jie Wang ◽  
Wenjin Liu
2020 ◽  
Vol 50 (9) ◽  
pp. 090013
Author(s):  
LiangFei GONG ◽  
Jie WANG ◽  
YiJiang XUE ◽  
RenRong LONG ◽  
TianFei REN ◽  
...  

2008 ◽  
Vol 385-387 ◽  
pp. 201-204
Author(s):  
Gong Shun Guan ◽  
Bao Jun Pang ◽  
Run Qiang Chi ◽  
Nai Gang Cui

In order to study the hypervelocity impact of space debris on spacecraft through hypervelocity impact on aluminum alloy multi-wall structure, a two-stage light gas gun was used to launch 2017-T4 aluminum alloy sphere projectiles. The projectile diameters ranged from 2.74mm to 6.35mm and impact velocities ranged from 1.91km/s to 5.58km/s. Firstly, the advanced method of multi-wall shield resisting hypervelocity impacts from space debris was investigated, and the effect of amount and thickness of wall on shield performance was discussed. Finally, by regression analyzing of experiment data, the experience equations for forecasting the diameter of the penetration hole on the first wall and the diameter of the damaged area on the second wall of aluminum multi-wall shield under hypervelocity normal impact of Al-spheres were obtained. The results indicated that the performance of multi-wall shield with more amount of wall is excellent when area density is constant. At the same time, intensity of the first wall and protecting space play the important roles.


2018 ◽  
Vol 183 ◽  
pp. 02033
Author(s):  
Masahiro Nishida ◽  
Fumiya Kodama ◽  
Koichi Hayashi ◽  
Yasuhiro Akahoshi ◽  
Kazuyuki Hokamoto ◽  
...  

Hypervelocity impact phenomena of long period stacking ordered type magnesium alloys (LPSO-Mg) plates were examined at the impact velocities of 4 km/s and 6 km/s. Ejecta veil and external bubble of debris of LPSO-Mg were darker than those of aluminum alloy A6061-T6. The size of external bubble of debris of LPSO-Mg was slightly smaller than that of A6061-T6. The velocity reduction of LPSOMg was slightly larger than that of A6061-T6. However, the scatter area of projectile and targets were not determined by electron probe micro-analyzer.


2014 ◽  
Vol 875-877 ◽  
pp. 1016-1020 ◽  
Author(s):  
Zhi Tao Tang ◽  
Tao Yu ◽  
Li Qiang Xu

The machining deformations caused by the release and redistribution of original residual stresses were studied by the theoretical analysis and finite element method. The research results show that the release and redistribution of original residual stresses result in machining distortion of the plate part. There exists an optimal value of material removal amount according to original residual stresses. When the amount of the material removed exceeds the optimal value, the machining deformation can be controlled effectively.


2011 ◽  
Vol 368-373 ◽  
pp. 253-257
Author(s):  
Yong Tao Gao ◽  
Ting He ◽  
Peng Bin Fu

For the aluminum alloy pipe stable form and buckling capacity, axis compressing test for 4 sections which each specification in three members, total 36 members, thus, we work out the ultimate bearing capacity for a little slenderness ratio alloy round pipe and relation between slenderness ratio and coefficient of stability, to provide test data for drawing pillars curve of the same type member. Through observed aluminum alloy compressing member changing with test process, record test phenomenon, and combined with instruments of test data record, providing the basis for further theoretical analysis.


2021 ◽  
Vol 13 (9) ◽  
pp. 168781402110491
Author(s):  
Kuo-Long Lee ◽  
Bo-You Liu ◽  
Wen-Fung Pan

This paper presents experimental study on the response of 6061-T6 aluminum alloy round-hole tubes with five different hole diameters of 2, 4, 6, 8, and 10 mm and four different diameter-to-thickness ratios of 30, 40, 50, and 60 submitted to pure bending creep and pure bending relaxation. Pure bending creep or relaxation is defined as bending the tube to the required moment or curvature and maintaining that moment or curvature for a period of time. The experimental results of pure bending creep show that the curvature increases with time. In addition, larger holding moment, diameter-to-thickness ratio, or hole diameter results in larger creep curvature. As the curvature continues to increase, the round-hole tube eventually breaks. The experimental results of pure bending relaxation show that the relaxation moment decreases sharply with time and tends to a stable value. In addition, larger holding curvature, diameter-to-thickness ratio, or hole diameter results in larger drop of the relaxation moment. Due to fixed curvature, the round-hole tube does not break. Finally, formulas proposed by the research team of Pan et al. were respectively improved to simulate the creep curvature-time relationship for pure bending creep in the initial and the secondary stages and the relaxation moment-time for pure bending relaxation. After comparing with the experimental results, it is found that theoretical analysis can reproduce the experimental results reasonably.


2014 ◽  
Vol 529 ◽  
pp. 153-158
Author(s):  
Jin Peng Yu ◽  
Li Min Zhang ◽  
Wei Hua Zhang ◽  
Xue Fei Huang ◽  
Guan Hua Huang

The results of the same modal analysis exhibit obvious diversity due to the different options of the finite element types and the modeling methods. Modal analysis was carried out on EMU aluminum alloy welded profile using finite element analysis, then mode shape and natural frequency of each model was abstracted, and then the results of simulation and experimental were contrastively analyzed. Based on these, a fast and reliable modeling method and a reasonable element type were obtained, which would be able to eliminate the blindness of the choice of modeling methods and element type, thus achieving a more reasonable theoretical analysis results that provide the reference for structure design and verification and the basis for improving the efficiency and precision of simulation analysis.


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