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

Publish Year: 1388
نوع سند: مقاله کنفرانسی
زبان: English
View: 1,730

This Paper With 8 Page And PDF Format Ready To Download

  • Certificate
  • من نویسنده این مقاله هستم

استخراج به نرم افزارهای پژوهشی:

لینک ثابت به این Paper:

شناسه ملی سند علمی:

AEROSPACE08_229

تاریخ نمایه سازی: 5 شهریور 1388

Abstract:

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.

Authors

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

مراجع و منابع این Paper:

لیست زیر مراجع و منابع استفاده شده در این Paper 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 Paper لینک شده اند :
  • 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