Transverse shear effects in supersonic flutter problems for composite multilayered rectangular plates - Benchmark for numerical analysis
Authors:
- Aleksander Muc
Abstract
To investigate the influence of transverse shear effects the present paper demonstrates the comparison of flutter characteristics for rectangular multilayered composite plates. The concise variational formulation is shown for various variants of the plate theories (classical, first order and higher order). The analytical, closed form solution is found for a specific boundary conditions dealing with two opposite edges being simply supported. The evaluated method of solution can be treated as the benchmark for numerical analysis since analytical results can be obtained directly with the use of the symbolic packages, such as Mathematica, Maple or Matlab.
- Record ID
- CUTd884988d87f64d4e9463658033a261ac
- Publication categories
- ;
- Author
- Journal series
- Composites Part C: Open Access, ISSN 2666-6820, e-ISSN 2666-6820
- Issue year
- 2020
- Vol
- 1
- Pages
- [1-5]
- Article number
- 100001
- Other elements of collation
- rys.; wykr.; Bibliografia (na s.) - [5]; Bibliografia (liczba pozycji) - 17; Oznaczenie streszczenia - Abstr.; Numeracja w czasopiśmie - Vol. 1
- Keywords in English
- transverse shear effects, supersonic flutter, analytical solutions, multilayerd composites, rectangular plates
- DOI
- DOI:10.1016/j.jcomc.2020.100001 Opening in a new tab
- URL
- https://www.sciencedirect.com/science/article/pii/S2666682020300013?via%3Dihub Opening in a new tab
- Language
- eng (en) English
- License
- Score (nominal)
- 5
- Uniform Resource Identifier
- https://cris.pk.edu.pl/info/article/CUTd884988d87f64d4e9463658033a261ac/
- URN
urn:pkr-prod:CUTd884988d87f64d4e9463658033a261ac
* presented citation count is obtained through Internet information analysis, and it is close to the number calculated by the Publish or PerishOpening in a new tab system.