A semi-analytical approach for linear and non-linear analysis of unstiffened laminated composite cylinders and cones under axial, torsion and pressure loads. (May 2015)
- Record Type:
- Journal Article
- Title:
- A semi-analytical approach for linear and non-linear analysis of unstiffened laminated composite cylinders and cones under axial, torsion and pressure loads. (May 2015)
- Main Title:
- A semi-analytical approach for linear and non-linear analysis of unstiffened laminated composite cylinders and cones under axial, torsion and pressure loads
- Authors:
- Castro, Saullo G.P.
Mittelstedt, Christian
Monteiro, Francisco A.C.
Arbelo, Mariano A.
Degenhardt, Richard
Ziegmann, Gerhard - Abstract:
- Abstract: A semi-analytical model for the non-linear analysis of simply supported, unstiffened laminated composite cylinders and cones using the Ritz method and the Classical Laminated Plate Theory is proposed. A matrix notation is used to formulate the problem using Donnell׳s and Sanders׳ non-linear equations. The approximation functions proposed are capable to simulate the elephant׳s foot effect, a common phenomenon and a common failure mode for cylindrical and conical structures under axial compression. Axial, torsion and pressure loads can be applied individually or combined, and solutions for linear static, linear buckling and non-linear buckling analyses are presented and verified using a commercial finite element software. The presented non-linear buckling analyses used perturbation loads to create the initial geometric imperfections, showing the capability of the method for arbitrary imperfection patterns. The linear stiffness matrices are integrated analytically and for the conical structures an approximation is proposed to overcome the non-integrable expressions. Highlights: A semi-analytical model for linear and non-linear buckling analysis is proposed. Axial compression, torsion, pressure and any additional forces can be applied to the shell surface. The elephant's foot effect, a common failure mode for cylinders and cones, is taken into account. Important implementation aspects are covered in the manuscript and the code is available on-line. The equations areAbstract: A semi-analytical model for the non-linear analysis of simply supported, unstiffened laminated composite cylinders and cones using the Ritz method and the Classical Laminated Plate Theory is proposed. A matrix notation is used to formulate the problem using Donnell׳s and Sanders׳ non-linear equations. The approximation functions proposed are capable to simulate the elephant׳s foot effect, a common phenomenon and a common failure mode for cylindrical and conical structures under axial compression. Axial, torsion and pressure loads can be applied individually or combined, and solutions for linear static, linear buckling and non-linear buckling analyses are presented and verified using a commercial finite element software. The presented non-linear buckling analyses used perturbation loads to create the initial geometric imperfections, showing the capability of the method for arbitrary imperfection patterns. The linear stiffness matrices are integrated analytically and for the conical structures an approximation is proposed to overcome the non-integrable expressions. Highlights: A semi-analytical model for linear and non-linear buckling analysis is proposed. Axial compression, torsion, pressure and any additional forces can be applied to the shell surface. The elephant's foot effect, a common failure mode for cylinders and cones, is taken into account. Important implementation aspects are covered in the manuscript and the code is available on-line. The equations are presented in matrix form and therefore can be easily applicable to other problems. … (more)
- Is Part Of:
- Thin-walled structures. Volume 90(2015)
- Journal:
- Thin-walled structures
- Issue:
- Volume 90(2015)
- Issue Display:
- Volume 90, Issue 2015 (2015)
- Year:
- 2015
- Volume:
- 90
- Issue:
- 2015
- Issue Sort Value:
- 2015-0090-2015-0000
- Page Start:
- 61
- Page End:
- 73
- Publication Date:
- 2015-05
- Subjects:
- Ritz method -- Linear buckling -- Linear static -- Non-linear analysis -- Cylinders -- Cones
Thin-walled structures -- Periodicals
690.1 - Journal URLs:
- http://www.sciencedirect.com/science/journal/02638231 ↗
http://www.elsevier.com/journals ↗ - DOI:
- 10.1016/j.tws.2015.01.002 ↗
- Languages:
- English
- ISSNs:
- 0263-8231
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 8820.121000
British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 6195.xml