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Parametric Studies and Numerical Analysis of Low Velocity Impact on Smart Hybrid Composite Laminates

Received: 7 September 2016     Accepted: 15 June 2017     Published: 31 July 2017
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Abstract

To evaluate the effect of low velocity impact on composite plate using nonlinear explicit finite element software LS-DYNA software. The theoretical basis of the present finite element model is verified by analyzing impact-loaded laminated composite plate previously been studied through analytical. The study of hybrid composite plates are carried were the SMA (shape memory alloy) are used in between the plies to increase the resistance. Also parametric studies were done to find the importance of the Mesh. The present numerical approach is successfully demonstrated through comparisons between experimentally-measured and computed force-time histories for impact of carbon fiber-reinforce plastic (CFRP) plates. Parametric studies are also conducted by varying Mesh results obtained are correlated with the results in the published literature.

Published in American Journal of Materials Synthesis and Processing (Volume 2, Issue 3)
DOI 10.11648/j.ajmsp.20170203.12
Page(s) 41-50
Creative Commons

This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.

Copyright

Copyright © The Author(s), 2017. Published by Science Publishing Group

Keywords

SMA, CFRP, Ls Dyna, Hypermesh, Low Velocity Impact, Belytschko-Tsay

References
[1] Vaziri. R, Quan. X and Olson. M. D “Impact analysis of laminated composite plates and shells by super finite elements Int. J. Impact Enon 9 Vol. 18, Nos 7 8, pp. 765-782, 1996.
[2] Shokuhfar. A, “Analysis and optimization of smart hybrid composite plates subjected to low-velocity impact using the response surface methodology (RSM)” Thin-Walled Structures 46 (2008) 1204–1212.
[3] SADIGHI. M, H. POURIAYEVALI, SAADATI. M “Response of fully backed sandwich beams to low velocity transverse impact” World Academy of Science, Engineering and Technology 36 2007.
[4] Hosur. M. V, “Studies on the low-velocity impact resip/;ponse of woven hybrid composites” Composite Structures 67 (2005) 253–262.
[5] Ik Hyeon Choi, “Low-velocity impact analysis of composite laminates using linearized contact law” Composite Structures 66 (2004) 125–132.
[6] Liu. G. R and Quek. S. S “The finite element method A practicle course”.
[7] LS-DYNA KEYWORD USER’S MANUAL”, Version-971, Livermore Software Technology Corporation, 2006.
[8] Tiebreak. R. a, Bachene. M b, Rechak S. c, Necib. B “Damage prediction in composite plates subjected to low velocity impact” Composite Structures 83 (2008) 73–82.
[9] Shiuh-Chuan Her, “The finite element analysis of composite laminates and shell structures subjected to low velocity impact” Composite Structures 66 (2004) 277–285.
[10] Zuleyha Aslan “The response of laminated composite plates under low-velocity impact loading” Composite Structures 59 (2003) 119–127.
[11] Krishnamurthy. K. S, “A parametric study of the impact response and damage of laminated cylindrical composite shells” Composites Science and Technology 61 (2001) 1655–1669.
[12] http://www.lsdyna.com
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  • APA Style

    Abdul Nazeer, Syed Kashif Hussain, Asif Iqbal M. Doddamani. (2017). Parametric Studies and Numerical Analysis of Low Velocity Impact on Smart Hybrid Composite Laminates. American Journal of Materials Synthesis and Processing, 2(3), 41-50. https://doi.org/10.11648/j.ajmsp.20170203.12

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    ACS Style

    Abdul Nazeer; Syed Kashif Hussain; Asif Iqbal M. Doddamani. Parametric Studies and Numerical Analysis of Low Velocity Impact on Smart Hybrid Composite Laminates. Am. J. Mater. Synth. Process. 2017, 2(3), 41-50. doi: 10.11648/j.ajmsp.20170203.12

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    AMA Style

    Abdul Nazeer, Syed Kashif Hussain, Asif Iqbal M. Doddamani. Parametric Studies and Numerical Analysis of Low Velocity Impact on Smart Hybrid Composite Laminates. Am J Mater Synth Process. 2017;2(3):41-50. doi: 10.11648/j.ajmsp.20170203.12

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  • @article{10.11648/j.ajmsp.20170203.12,
      author = {Abdul Nazeer and Syed Kashif Hussain and Asif Iqbal M. Doddamani},
      title = {Parametric Studies and Numerical Analysis of Low Velocity Impact on Smart Hybrid Composite Laminates},
      journal = {American Journal of Materials Synthesis and Processing},
      volume = {2},
      number = {3},
      pages = {41-50},
      doi = {10.11648/j.ajmsp.20170203.12},
      url = {https://doi.org/10.11648/j.ajmsp.20170203.12},
      eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ajmsp.20170203.12},
      abstract = {To evaluate the effect of low velocity impact on composite plate using nonlinear explicit finite element software LS-DYNA software. The theoretical basis of the present finite element model is verified by analyzing impact-loaded laminated composite plate previously been studied through analytical. The study of hybrid composite plates are carried were the SMA (shape memory alloy) are used in between the plies to increase the resistance. Also parametric studies were done to find the importance of the Mesh. The present numerical approach is successfully demonstrated through comparisons between experimentally-measured and computed force-time histories for impact of carbon fiber-reinforce plastic (CFRP) plates. Parametric studies are also conducted by varying Mesh results obtained are correlated with the results in the published literature.},
     year = {2017}
    }
    

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  • TY  - JOUR
    T1  - Parametric Studies and Numerical Analysis of Low Velocity Impact on Smart Hybrid Composite Laminates
    AU  - Abdul Nazeer
    AU  - Syed Kashif Hussain
    AU  - Asif Iqbal M. Doddamani
    Y1  - 2017/07/31
    PY  - 2017
    N1  - https://doi.org/10.11648/j.ajmsp.20170203.12
    DO  - 10.11648/j.ajmsp.20170203.12
    T2  - American Journal of Materials Synthesis and Processing
    JF  - American Journal of Materials Synthesis and Processing
    JO  - American Journal of Materials Synthesis and Processing
    SP  - 41
    EP  - 50
    PB  - Science Publishing Group
    SN  - 2575-1530
    UR  - https://doi.org/10.11648/j.ajmsp.20170203.12
    AB  - To evaluate the effect of low velocity impact on composite plate using nonlinear explicit finite element software LS-DYNA software. The theoretical basis of the present finite element model is verified by analyzing impact-loaded laminated composite plate previously been studied through analytical. The study of hybrid composite plates are carried were the SMA (shape memory alloy) are used in between the plies to increase the resistance. Also parametric studies were done to find the importance of the Mesh. The present numerical approach is successfully demonstrated through comparisons between experimentally-measured and computed force-time histories for impact of carbon fiber-reinforce plastic (CFRP) plates. Parametric studies are also conducted by varying Mesh results obtained are correlated with the results in the published literature.
    VL  - 2
    IS  - 3
    ER  - 

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Author Information
  • Department of Mechanical Engineering, Khaja Bandanawaz College of Engineering, Gulbarga, India

  • Department of Mechanical Engineering, Khaja Bandanawaz College of Engineering, Gulbarga, India

  • Department of Mechanical Engineering, SECAB Institute of Engineering & Technology, Bijapur, India

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