Buckling Analysis of Variable Stiffness Composite Cylindrical Shells Based on Hermite Curves

Article Preview

Abstract:

Based on the Hermite curve, the buckling behavior of a variable stiffness composite cylindrical shell is investigated. Firstly, the cylindrical shell is unfolded into a plane, and the Hermite curve is taken as the basic reference path on the plane and the variation of the fiber orientation is obtained. Then, the finite element analysis pre-processing program of the variable stiffness composite cylindrical shell is written by Python to develop ABAQUS interactive interface. Finally, the GUI plug-in is developed successfully, the buckling analysis of the constant stiffness and variable stiffness cylindrical shells is carried out and the effect of buckling load on the initial tangential direction q1, the initial point tangential magnitude L1, the end point tangential direction q2, the end point tangential magnitude L2 is preliminarily explored. It is found that the buckling load of the variable stiffness cylindrical shell is improved greatly. The secondary development of ABAQUS by Python is used to realize the automatic modeling and calculation analysis of the variable stiffness cylindrical shell parts, which provides research ideas and processes for practical engineering research, and has certain practical significance.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

191-197

Citation:

Online since:

June 2019

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2019 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] M. Wu, Y. Gao, Y. Cheng, B. Wang, T. Huo. Carbon Fiber Composite Materials Finite Element Simulation Analysis of Cutting Force. Proc. Cirp, 56 (2016) 109-114.

DOI: 10.1016/j.procir.2016.10.031

Google Scholar

[2] T. Roberts, Rapid growth forecast for carbon fiber market. Reinforced Plast. 51(2) 10-13.

Google Scholar

[3] Z. Gürdal, R. Olmedo, In-plane response of laminates with spatially varying fiber orientations: Variable stiffness concept. AIAA J. 31(4) 751-758.

DOI: 10.2514/3.11613

Google Scholar

[4] Z. Gürdal, B. F. Tating, K. C. Wu, Variable stiffness composite panels: Effects of stiffness variation on the in-plane buckling response. Comp. Part A: Appl. Sci. Manuf. 39 (2008) 911-922.

DOI: 10.1016/j.compositesa.2007.11.015

Google Scholar

[5] M. Hyer, H. Lee, The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes. Compos. Struct. 18 (3) (1991) 239-261.

DOI: 10.1016/0263-8223(91)90035-w

Google Scholar

[6] C. S. Lopes, Z. Gürdal, P. P. Camanho, Variable-stiffness Composite Panels: Buckling and First-ply Failure Improvements over Straight-fibre Laminates. Comp. Struct. 86(9) 897-970.

DOI: 10.1016/j.compstruc.2007.04.016

Google Scholar

[7] C. Waldhart, Z. Gürdal, C. Ribbens. Analysis of Tow Placed, Parallel Fiber, Variable Stiffness Laminates. In Proceedings of the 37th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials (SDM) Conference, Salt Lake City, UT, USA, (1996).

DOI: 10.2514/6.1996-1569

Google Scholar

[8] C. Waldhart. Analysis of Tow-placed, Variable-stiffness Laminates. Master thesis, Virginia Polytechnic Institute and State University, June (1996).

Google Scholar

[9] A. W. Blom, Structural Performance of Fiber-placed Variable-stiffness Composite Conical and Cylindrical Shells. Netherlands: Delft University of Technology, 2010 31-56.

Google Scholar

[10] Z. M. Wu, P. W. Weaver,G. Raju, et al. Buckling Analysis and Optimization of Variable Angle Tow Composite Plates. Thin-walled Struct. 60 (2012) 163-172.

DOI: 10.1016/j.tws.2012.07.008

Google Scholar

[11] H. Akhavan, P. Ribeiro, Natural Modes of Vibration of Variable Stiffness Composite Laminates with Curvilinear Fibers. Comp. Struct. 93(11) 3040-3047.

DOI: 10.1016/j.compstruct.2011.04.027

Google Scholar

[12] S. Nagendra, S. Kodiyalam, J. Davis, V. Parthasarathy, Optimization of tow fiber paths for composite design. Proceedings of the AIAA/ASME/ASCE/AHS/ASC 36th Structures, Structural Dynamics and Materials Conference. New Orleans, LA, 1995, 1031-1041.

DOI: 10.2514/6.1995-1275

Google Scholar

[13] M. W. Paul, D. P. Kevin, Buckling of Variable Angle Tow Plates: from Concept to Experiment, 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 17th, Palm Springs, California.

DOI: 10.2514/6.2009-2509

Google Scholar

[14] A. Alhajahmad, M. M. Abdalla, Z. Gürdal, Design tailoring for pressure pillowing using tow-placed steered fibers. J. Aircraft, 45(2) 630-640.

DOI: 10.2514/1.32676

Google Scholar

[15] S. Setoodeh, et al., Design of variable-stiffness composite panels for maximum buckling load. Compos. Struct. 87(1) 109–117.

DOI: 10.1016/j.compstruct.2008.01.008

Google Scholar

[16] H. Y. Fu, Z. L. Cao, L. Du, et al, Design of Bezier curve variable angle laminates and analysis on bulking property Acta Mater. Composit. Sin. 34(8) 1729-1735(in Chinese).

Google Scholar

[17] A. Marouene, R. Boukhili, J. Chen, et al. Effects of gaps and overlaps on the buckling behavior of an optimally designed variable-stiffness composite laminates–a numerical and experimental study. Comp. Struct. 140 (2016) 556-566.

DOI: 10.1016/j.compstruct.2016.01.012

Google Scholar

[18] O. Falcó, J. A. Mayugo, C. S. Lopes, et al. Variable-stiffness composite panels: As-manufactured modeling and its influence on the failure behavior. Comp. Part B: Eng. 56 (2014) 660-669.

DOI: 10.1016/j.compositesb.2013.09.003

Google Scholar

[19] M. Arian Nik, K. Fayazbakhsh, D. Pasini, et al. A comparative study of metamodeling methods for the design optimization of variable stiffness composites. Comp. Struct. 107 (2014) 494-501.

DOI: 10.1016/j.compstruct.2013.08.023

Google Scholar

[20] A. H. Akbarzadeh, M. Arian Nik, D. Pasini. Vibration responses and suppression of variable stiffness laminates with optimally steered fibers and magnetostrictive layers. Comp. Part B: Eng. 91 (2016) 315-326.

DOI: 10.1016/j.compositesb.2016.02.003

Google Scholar