Numerical Investigation of the Grid Geometry Effect on the Modal Response and Buckling of Grid-Stiffened Composite Conical Structure

Publish Year: 1400
نوع سند: مقاله ژورنالی
زبان: English
View: 253

This Paper With 5 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:

JR_ADMTL-14-3_010

تاریخ نمایه سازی: 1 آبان 1400

Abstract:

This study aims to the investigation of the effect of grid geometry on the modal response and buckling strength of a composite conical lattice structure under static axial loading by Finite Element Method (FEM). For this purpose, four structures with similar geometry have been designed through four grid structures. Abaqus finite element software has been used for modeling and analyzing the structures. The experimental results of Zamani and Ahmadifar study [۱] have been used to validate the results of FEM. Given the results of numerical and experimental analysis, there is an accordance between the results and the FEM efficiency. The results show the contiguous natural frequency of the structures so that their negligible difference is due to the variations of structures’ weight and stiffness. Changing the grid does not affect the shape of the modes. The isogrid bears a higher buckling loading than the anisogrid. Reducing the rib angle is an effective parameter, which increases the buckling loading on the structure. Although peripheral ribs play a role in load bearing, adding their numbers increases the total weight of the structure, therefore, it has no significant effect on increasing the stability of the structure.

Keywords:

Grid-stiffened composite conical structure , FEM , Modal Analysis , Buckling

Authors

Mohammad Reza Zamani

Department of Mechanical Engineering, Malek Ashtar University of Technology, Tehran, Iran

Mohsen Zaretabar

Department of Mechanical Engineering, Malek Ashtar University of Technology, Tehran, Iran

Hossein Parsa

Department of Mechanical Engineering, Malek Ashtar University of Technology, Tehran, Iran

Mohsen Heydari Beni

Department of Mechanical Engineering, Malek Ashtar University of Technology, Tehran, Iran

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 :
  • Ahmadifar, A., Zamani, M. R., Davar, A., Eskandari Jam, J., ...
  • Vasiliev, V., Razin, A., Anisogrid Composite Lattice Structures for Spacecraft ...
  • Totaro, G., Flexural, Torsional, and Axial Global Stiffness Properties of ...
  • Mangas, C., Vilanova, J., Díaz, V., Samartín, C., Kiryenko, S., ...
  • Khadem, S. E., Nezamoleslami, R., Investigation of the Free Vibrations ...
  • Davar, A., Azarafza, R., and Bagheri, V., Experimental and Numerical ...
  • نمایش کامل مراجع