Refine your search
Collections
Co-Authors
Year
A B C D E F G H I J K L M N O P Q R S T U V W X Y Z All
Suleiman, Osama Mohammed Elmardi
- Effect of Lamination Scheme on Buckling Load for Laminated Composite Decks Plates
Abstract Views :188 |
PDF Views:0
Authors
Affiliations
1 Department of Mech. Engg., Nile Valley University, Atbara, River Nile, SD
2 Department of Mech. Engg., Kassala University, Kassala, SD
3 Department of Mech. Engg., Omdurman Islamic University, Omdurman, Khartoum, SD
1 Department of Mech. Engg., Nile Valley University, Atbara, River Nile, SD
2 Department of Mech. Engg., Kassala University, Kassala, SD
3 Department of Mech. Engg., Omdurman Islamic University, Omdurman, Khartoum, SD
Source
International Journal of System & Software Engineering, Vol 7, No 1 (2019), Pagination: 20-27Abstract
New numerical results are generated for in-plane compressive biaxial buckling which serve to quantify the effects of lamination scheme on buckling loading. The results indicate that the symmetric laminate is stiffer than the anti-symmetric one. This phenomenon is caused by coupling between bending and stretching which lowers the buckling loads of symmetric laminate.Keywords
Biaxial Buckling, Classical Laminated Plate Theory, Composite Laminated Decks Plates, Finite Element, Fortran Program, Lamination Scheme.
References
- G. J. Turvey, and M. Y. Osman, “Elastic large deflection analysis of isotropic rectangular Mindlin plates,” International Journal of Mechanical Sciences, vol. 22; pp. 1-14, 1990.
- G. J. Turvey, and M. Y. Osman, “Large deflection analysis of orthotropic Mindlin plates,” Proceedings of the 12th Energy Resource Technology Conference and Exhibition, Houston, Texas, pp. 163-172, 1989.
- G. J. Turvey, and M. Y. Osman, “Large deflection effects in anti-symmetric cross-ply laminated strips and plates,” in I. H. Marshall, (eds), Composite Structures, vol. 6, Paisley College, Scotland, Elsevier Science Publishers, pp. 397-413, 1991.
- O. M. E. Suleiman, “Verification of Dynamic Relaxation (DR) method in isotropic, orthotropic and laminated plates using small deflection theory,” International Journal of Advanced Science and Technology, vol. 72, pp. 37-48, 2014.
- O. M. E. Suleiman, “Nonlinear analysis of rectangular laminated plates using large deflection theory,” International Journal of Emerging Technology and Research, vol. 2, no. 5, pp. 26-48, 2015.
- O. M. E. Suleiman, ‘Validation of Dynamic Relaxation (DR) method in rectangular laminates using large deflection theory,” International Journal of Advanced Research in Computer Science and Software Engineering, vol. 5, no. 9, pp. 137-144, September 2015.
- O. M. E. Suleiman, Nonlinear Analysis of Rectangular Laminated Plates, Lap Lambert Academic Publishing, Germany, 2015.
- O. M. E. Suleiman, Text Book on Dynamic Relaxation Method, Lap Lambert Academic Publishing, Germany, 2016.
- L. J. Segelind, Applied Finite Element Analysis, John Wiley and Sons’ Publishers, 1984.
- A. W. Al-Khafaji, and J. R. Tooley, Numerical Methods in Engineering Practice, CBS Publishing Japan Ltd, 1986.
- T. D. Eastop, and A. McConkey, Applied Thermodynamics for Engineering Technologists, 5th ed., John Wiley and Sons, New York, 1993.
- O. M. E. Suleiman, Introduction and Literature Review on Buckling of Composite Laminated Plates, Lap Lambert Academic Publishing, Germany, 2016.
- O. M. E. Suleiman, “Bibliography and literature review on buckling of laminated plates,” International Journal of Science and Engineering, vol. 2, no. 8, pp. 104-112, August 2016.