Numerical simulation on high speed impact behavior of Al-W and Al-Ni mixture

2018 ◽  
Vol 32 (10) ◽  
pp. 4629-4636
Author(s):  
Kyungsun Chung ◽  
Hyoungjoon Kwon ◽  
Jung Su Park ◽  
Soonho Song
2019 ◽  
Vol 811 ◽  
pp. 151875 ◽  
Author(s):  
Pengcheng Guo ◽  
Luoxing Li ◽  
Gang Xiao ◽  
Shufen Cao ◽  
Guan Wang ◽  
...  

Author(s):  
Rahul Dubey ◽  
Raja Allavikutty ◽  
R. Velmurugan ◽  
R. Jayaganthan

Abstract Aluminium alloy AA 6082-T6 was rolled at cryogenic and room temperatures to final thickness of 0.5 mm after 75% thickness reduction and subjected to high speed impact. The deformed alloy was investigated for its ballistic properties due to potential applications in aerospace and automotive sectors. The cryogenic and room temperature rolled samples were subjected to normal high-speed impact using a gas gun arrangement to shoot nosed projectiles at velocities higher than the ballistic limits. Phantom ‘V611’ high-speed camera was used to measure the initial and residual velocities of the projectile. Nano-indentation was performed to relate hardness of the initial sample with the observed impact behaviour. Detailed fractographic studies were conducted using Scanning Electron Microscopy (SEM) to substantiate the possible failure mechanisms upon impact. Electron Backscatter Diffraction (EBSD) and Energy Dispersive X-ray Spectroscopy (EDS) were used to characterize the microstructure of the deformed samples. The high speed impact data is correlated with the metallographic observations in this study.


2019 ◽  
Vol 11 (5) ◽  
pp. 723-736
Author(s):  
Radek Doubrava ◽  
Martin Oberthor ◽  
Petr Bělský ◽  
Jan Raška

Purpose The purpose of this paper is to describe the approach for the design of a jet engine composite air inlet for a new generation of jet trainer aircraft from the perspective of airworthiness requirements regarding high-speed impact resistance. Design/methodology/approach Validated numerical simulation was applied to flat test panels. The final design was optimised and verified by validated numerical simulation and verified by testing on a full-scale demonstrator. High-speed camera measurement and non-destructive testing (NDT) results were used for the verification of the numerical models. Findings The test results of flat test panels confirmed the high durability of the composite structure during inclined high-speed impact with a near-real jet inlet load boundary condition. Research limitations/implications Owing to the sensitivity of the composite material on technology production, the results are limited by the material used and the production technology. Practical implications The application of flat test panels for the verification and tuning of numerical models allows optimised final design of the air inlet and reduces the risk of structural non-compliance during verification tests. Originality/value Numerical models were verified for simulation of the real composite structure based on high-speed camera results and NDT inspection after impact. The proposed numerical model was simplified for application in a real complex design and reduced calculation time.


2020 ◽  
Vol 303 ◽  
pp. 1-7
Author(s):  
E.N. Kramshonkov ◽  
A.V. Krainov ◽  
Evgeny N. Pashkov

The paper discusses the results of the numerical simulation of high-speed impact effect of compact projectiles made of steel and tungsten alloy with steel obstacles of equal mass. The obstacles have different initial porosity of the material. Conducted the final evaluation of the penetration speed of the projectile depending on the porosity of the obstacle and the initial speed of the shock interaction. The initial impact velocity range from 1 to 16 [km/s]. The destruction, melting and evaporation of the interacting bodies are taken into account. The analysis of porosity influence evaluation of obstacles material revealed that the protective advantage of porous obstacles disclose at the higher impact velocities, greater than 1.5 [km/s] for steel strikers and 2 [km/s] for projectiles of tungsten alloy. The more impact velocity the more protective effect of porous obstacles.


2015 ◽  
Vol 25 (2) ◽  
pp. 559-570
Author(s):  
Wei-gui ZHANG ◽  
Liang-ju HE ◽  
Pei-jie LI ◽  
Yi-cong YE ◽  
Xue FENG ◽  
...  

2021 ◽  
Vol 30 (3) ◽  
pp. 503-522 ◽  
Author(s):  
Bahman Daneshian ◽  
Frank Gaertner ◽  
Hamid Assadi ◽  
Daniel Hoeche ◽  
Wolfgang Weber ◽  
...  

AbstractUp to now, the role of particle sizes on the impact behavior of ceramic particles in aerosol deposition not yet fully understood. Hence, with the aim to supply a more general understanding, modeling series of low strain rate compression and high-speed impact were performed by molecular dynamics on single-crystalline particles in sizes of 10-300 nm that are tuned to match mechanical properties of TiO2-anatase. The modeling results reveal that particles with original diameter of 25-75 nm exhibit three different impact behaviors that could be distinguished as (i) rebounding, (ii) bonding and (iii) fragmentation, depending on their initial impact velocity. In contrast, particles larger than 75 nm do not exhibit the bonding behavior. Detailed stress and strain field distributions reveal that combination of “localized inelastic deformation” along the slip systems and “shear localization” cause bonding of the small and large particles to the substrate. The analyses of associated temperature rise by the inelastic deformation revealed that heat diffusion at these small scales depend on size. Whereas small particles could reach a rather homogeneous temperature distribution, the evolved heat in the larger ones keeps rather localized to areas of highest deformation and may support deformation and the formation of dense layers in aerosol deposition.


2020 ◽  
Vol 29 (10) ◽  
pp. 6427-6438
Author(s):  
Guangli Bi ◽  
Zuocheng Xu ◽  
Jing Jiang ◽  
Yuandong Li ◽  
Tijun Chen ◽  
...  

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