Numerical Analysis of Ti/APC-2 Hybrid Composite Laminates after High-Velocity Impact

碩士 === 國立中山大學 === 機械與機電工程學系研究所 === 101 === This paper aims to investigate the failure analysis of Ti/APC-2 anisotropic composite laminates after high-velocity impact. The ANSYS/LS-DYNA software was used to simulate the high-velocity impact process. Then, compare the theoretical calculations with the...

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Main Authors: Shang-Meng Liu, 劉上盟
Other Authors: Ming-Hwa R. Jen
Format: Others
Language:zh-TW
Published: 2013
Online Access:http://ndltd.ncl.edu.tw/handle/88720708579305226534
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spelling ndltd-TW-101NSYS54900302015-10-13T22:40:48Z http://ndltd.ncl.edu.tw/handle/88720708579305226534 Numerical Analysis of Ti/APC-2 Hybrid Composite Laminates after High-Velocity Impact 鈦合金/碳纖維/聚醚醚酮混合型複合材料積層板承受高速衝擊後之數值分析 Shang-Meng Liu 劉上盟 碩士 國立中山大學 機械與機電工程學系研究所 101 This paper aims to investigate the failure analysis of Ti/APC-2 anisotropic composite laminates after high-velocity impact. The ANSYS/LS-DYNA software was used to simulate the high-velocity impact process. Then, compare the theoretical calculations with the numerical simulation results of ballistic limit in the Ti/APC-2 laminates to confirm the reliability of simulation. The analysis includes failure mode of laminates, projectile velocity and energy changes, the internal energy of laminate, and the changes by using different lay-ups or material. The main work can be divided into two parts: the first part is presentation of ANSYS/LS-DYNA simulation processes and results. High-velocity impact will be acted on the simulation samples, which are 3, 5, 9, 17, and 25 lay-ups laminates with 100, 200, 500, 1000, 1500, and 2000 m/s projectile velocities, respectively. Second, the ballistic limit was obtained by theoretical calculation. Then, the simulations results were compared and discussed. By comparing the theoretical calculations with the simulation results of ballistic limit in the Ti/APC-2 laminates, the errors of simulation results are quite acceptable, i.e., the reliability of simulation is in good agreement. If the initial velocity of projectile is close to ballistic limit, the influence of structural damage, internal energy absorption, and changes of projectile velocity and energy are more obvious. After impact, absorption of internal energy of Ti sheet is much larger than APC-2, and the backsheet of Ti absorb more energy than facesheet of Ti usually. Under the same material composition, the more stratified laminates possess better impact resistance. Replace a portion of Ti sheets with Al sheets, the impact resistance do not increase. Ming-Hwa R. Jen 任明華 2013 學位論文 ; thesis 84 zh-TW
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language zh-TW
format Others
sources NDLTD
description 碩士 === 國立中山大學 === 機械與機電工程學系研究所 === 101 === This paper aims to investigate the failure analysis of Ti/APC-2 anisotropic composite laminates after high-velocity impact. The ANSYS/LS-DYNA software was used to simulate the high-velocity impact process. Then, compare the theoretical calculations with the numerical simulation results of ballistic limit in the Ti/APC-2 laminates to confirm the reliability of simulation. The analysis includes failure mode of laminates, projectile velocity and energy changes, the internal energy of laminate, and the changes by using different lay-ups or material. The main work can be divided into two parts: the first part is presentation of ANSYS/LS-DYNA simulation processes and results. High-velocity impact will be acted on the simulation samples, which are 3, 5, 9, 17, and 25 lay-ups laminates with 100, 200, 500, 1000, 1500, and 2000 m/s projectile velocities, respectively. Second, the ballistic limit was obtained by theoretical calculation. Then, the simulations results were compared and discussed. By comparing the theoretical calculations with the simulation results of ballistic limit in the Ti/APC-2 laminates, the errors of simulation results are quite acceptable, i.e., the reliability of simulation is in good agreement. If the initial velocity of projectile is close to ballistic limit, the influence of structural damage, internal energy absorption, and changes of projectile velocity and energy are more obvious. After impact, absorption of internal energy of Ti sheet is much larger than APC-2, and the backsheet of Ti absorb more energy than facesheet of Ti usually. Under the same material composition, the more stratified laminates possess better impact resistance. Replace a portion of Ti sheets with Al sheets, the impact resistance do not increase.
author2 Ming-Hwa R. Jen
author_facet Ming-Hwa R. Jen
Shang-Meng Liu
劉上盟
author Shang-Meng Liu
劉上盟
spellingShingle Shang-Meng Liu
劉上盟
Numerical Analysis of Ti/APC-2 Hybrid Composite Laminates after High-Velocity Impact
author_sort Shang-Meng Liu
title Numerical Analysis of Ti/APC-2 Hybrid Composite Laminates after High-Velocity Impact
title_short Numerical Analysis of Ti/APC-2 Hybrid Composite Laminates after High-Velocity Impact
title_full Numerical Analysis of Ti/APC-2 Hybrid Composite Laminates after High-Velocity Impact
title_fullStr Numerical Analysis of Ti/APC-2 Hybrid Composite Laminates after High-Velocity Impact
title_full_unstemmed Numerical Analysis of Ti/APC-2 Hybrid Composite Laminates after High-Velocity Impact
title_sort numerical analysis of ti/apc-2 hybrid composite laminates after high-velocity impact
publishDate 2013
url http://ndltd.ncl.edu.tw/handle/88720708579305226534
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