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Analysis of axisymmetric laminated composite shells subjected to asymmetric loading
| Content Provider | Semantic Scholar |
|---|---|
| Author | Upadhya, A. K. Aruna, Hm |
| Copyright Year | 1986 |
| 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. |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | https://nal-ir.nal.res.in/3327/1/analysis_of_axisymmetric.pdf |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |
