Effects of Different Boundary Conditions on Free vibration Response of Sandwich Panels with flexible core and Distributed Attached Mass

سال انتشار: 1388
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 1,780

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شناسه ملی سند علمی:

AEROSPACE08_229

تاریخ نمایه سازی: 5 شهریور 1388

چکیده مقاله:

The free vibration analysis of rectangular sandwich panels with a flexible core both without and with a uniformly distributed attached mass on the top face sheet is carried out using the Finite Element Method through APDL (ANSYS Parametric Design Language) which is validated by several literatures through some numerical examples. The validated finite element model is then used to study the effect of different boundary conditions for both the top and the botton face sheets of sandwich panels without and with distributed attached mass on the natural frequencies of the sandwich panel as well as the normal and shear stresses. Numerical results that hitherto not reported in the literature have been presented in this paper. The results presented in this investigation could be useful to acquire a better insight into the behavior of sandwich laminates carrying attached mass for engineering designers of sandwich structures. The results are presented and compared with the latest numerical results found in literature.

نویسندگان

K. MALEKZADEH

Assistant Professor, Mechnical Engineering Departmetn, Malek e Ashtar University of Technology.Department of Mechanical Engineering, Malek Ashtar University of Technology

A. SAYYIDMOUSAVI

MSc Engineer, Mechanical Engineering Department, Khajeh Nasir Toosi University of Technology, Department of Mechanical Engineering, K.N. Tossi University of Technology

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  • Noor AK, Butom WS, Bert CW, (1996). shells. dف Computatiobal ...
  • _ Cha K.T, Leung T.P, Wong W.O, (1996). Free vibration ...
  • Chan K.T, Wang X.O, (199). Free vibration of Timosbeko beam ...
  • Rossi R.E, Laua P.A.A, (1996). Symmetric aad ati symmetric nomal ...
  • _ Sheikh A.H, Halder S, Sengupta D, (2004). Free flexura] ...
  • Tongan Waog, ladiir Sokoliasky, Shabkar Rajaram, Steve R. Nutt (2008). ...
  • r-- Reddy J.N, (1997). Mechabics of Labrated Composite Plates, Theory ...
  • Matbews FL, Davies G.A.O, Hitchings D, S5utis C, (2000)Finite element ...
  • _ KJause-Jurgun Bathe, (1996). Finite Element Procedures. Prentice Hall _ ...
  • Frostig Y, Bach M, (1994). Free Vibatios o Beams with ...
  • Frostig Y, (1998). Bucklog of sandwich plates _ a flexible ...
  • Frostig Y, Thomsen O.T, (2004). Higher order fee vibration of ...
  • Mijia Y, Pizhong Q, (2005). Higher order theory ibpact bodeling ...
  • Malekzadeh K, Khalili M.R, Mittal R.K, (2005). Lccal and Global ...
  • Malekzadeh K, Khalili M.R, Olsso R, Jafari A, (2006). Higher ...
  • Nayak A.K, Moy S.S.J, Shenoi R.A. (2002). Free vibration analysis ...
  • _ Khatua TP, Cheung YK, (1972). Triangular elemebt for bulti-layer ...
  • _ Sbeikb A.H, Halder S, Sepgupta D, (2002). Vibration of ...
  • نمایش کامل مراجع