Effect of Delamination Size and Location on Natural Frequency ofLaminated Composite Beams Using Finite Element Method

سال انتشار: 1392
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 1,313

فایل این مقاله در 6 صفحه با فرمت PDF قابل دریافت می باشد

استخراج به نرم افزارهای پژوهشی:

لینک ثابت به این مقاله:

شناسه ملی سند علمی:

WMECH02_138

تاریخ نمایه سازی: 21 تیر 1393

چکیده مقاله:

Detection of delamination in laminated composite structures is great of interest to engineers from the reliability point of view. Vibration-based methods which investigate changes in vibration characteristics (especially natural frequencies) of a structure due to damage are highly promising in this regard. Therefore, a procedure based on the natural frequency is developed in this study to detect the existence of delamination in laminated composite beams and then specify the size and location of delamination.In fact, delaminated composite beams with different size and location of delaminations are modeled in commercial finite element software, ABAQUS, and natural frequencies are extracted from the modal analysis. The numerical results are validated by analytical and experimental results available in the literature. Finally, a database is generated for different sizes and locations of delamination in laminated beams versus natural frequency. An engineer can predict the frequency behavior of a delaminated beam by changing the size and location of delamination.

کلیدواژه ها:

Composite beams ، delamination detection ، free vibration ، finite element method (FEM)

نویسندگان

K Torabi

Assistant Professor

M Shariati Nia

PhD Student, Department of Mechanical Engineering, University of Kashan, Kashan, ۸۷۳۱۷۵۱۱۶۷, Iran

M Heidari-Rarani

Assistant Professor, Faculty of Engineering, University of Isfahan, Isfahan, Iran

مراجع و منابع این مقاله:

لیست زیر مراجع و منابع استفاده شده در این مقاله را نمایش می دهد. این مراجع به صورت کاملا ماشینی و بر اساس هوش مصنوعی استخراج شده اند و لذا ممکن است دارای اشکالاتی باشند که به مرور زمان دقت استخراج این محتوا افزایش می یابد. مراجعی که مقالات مربوط به آنها در سیویلیکا نمایه شده و پیدا شده اند، به خود مقاله لینک شده اند :
  • Ramkumar, R.L. et al. (1979), 34th Annual Technical Conference, 1979 ...
  • Wang, J.T.S. et al. (1982), Journal of Sound and Vibrations ...
  • Mujumdar, P.M. and Suryanarayan, S., (1988), Journal of Sound and ...
  • Shen, M.-H.H. and Grady, J.E., (1992), AIAA Journal 30(5), pp. ...
  • Hu, J.S. and Hwu, C., (1995), AIAA Journal 33(10), pp. ...
  • Lee, J., (2000), Computers and Structures 74, pp. 121-129. ...
  • Zou, Y. et al. (2000), Journal of Sound and Vibration ...
  • Luo, H. and Hanagud, S., (2000), International Journal of Solids ...
  • Karmakar, A. et al. (2005), Aircraft Engineering and Aerospace Technology ...
  • Della, C.N. and Shu, D., (2007), Applied Mechanics Reviews 60(1), ...
  • Della, C.N. and D. Shu, D., (2009), Journal of Reinforced ...
  • Ramtekkar, G.S., (2009), Journal of Sound and Vibration 328, pp. ...
  • Shu, D. and Della, C.N., (2004), Compos Struct 64(3-4), pp. ...
  • Shu, D. and Della, C.N., (2004), Int J MechSct 46(4), ...
  • Della, C.N. and Shu, D., (2005), Eur J MechA 24(3), ...
  • نمایش کامل مراجع