Upadhya, AR and Aruna, HM (1986) Analysis of axisymmetric laminated composite shells subjected to asymmetric loading. Journal of Aeronautical Society of India, 38 (3). pp. 93-103.
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) |
PDF
analysis_of_axisymmetric.pdf Download (1MB) |
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/other.png) |
Indexer Terms (Generate index codes conversion from application/pdf to indexcodes)
indexcodes.txt Download (9kB) |
Abstract
A finite element formulation for the static analysis of a laminated composite shell of revolution with general meridional curvature, subjected to asymmetric loading, is presented. The analysis uses an axisymmetric laminated shell element where the shell geometry is satisfactorily represented; higher order polynomial approximations are used for the displacement fields. The asymmetric loading problem is handled through a Fourier series representation of the applied loads and the resultant displacements. Solutions are presented for typical aerospace shell structures like a composite cone and a tangent ogive shell subjected to wind loads.
| Item Type: | Article |
|---|---|
| Uncontrolled Keywords: | Shells (structural forms);Asymmetry;Displacement; Aeronautics;Approximation;Aerospace;Formulations;Finite element method;Curvature;Statics;Ogives;Aircraft components; Composite structures;Conical shells;Ogives;Static loads; Structural analysis;Fourier series;Laminates |
| Subjects: | ENGINEERING > Structural Mechanics AERONAUTICS > Aeronautics (General) |
| Depositing User: | Mr. Ravikumar R |
| Date Deposited: | 08 Nov 2006 |
| Last Modified: | 24 May 2010 04:23 |
| URI: | http://nal-ir.nal.res.in/id/eprint/3327 |
Actions (login required)
 |
View Item |
