Back
Analytical solutions of supersonic flutter problems for laminated multilayered composite plates and cylindrical shells
Authors:
- Justyna Flis,
- Aleksander Muc
Abstract
For laminated rectangular plates and cylindrical shells the analytical, closed form solution is found using classical and first order transverse shear formulations of kinematical hypothesis. The analysis is carried out 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
- CUT7ded3381bae343ecabbb0d0d316d1406
- Publication categories
- ;
- Author
- Journal series
- Vibrations in Physical Systems, ISSN 0860-6897
- Issue year
- 2020
- Vol
- 31
- No
- 3
- Pages
- [1-8]
- Article number
- 2020305
- Other elements of collation
- rys.; tab.; wykr.; Bibliografia (na s.) - 6-7; Bibliografia (liczba pozycji) - 12; Oznaczenie streszczenia - Abstr.; Numeracja w czasopiśmie - Vol. 31, No. 3
- Keywords in English
- flutter, multilayered laminated structures, plates, cylindrical shells
- DOI
- DOI:10.21008/j.0860-6897.2020.3.05 Opening in a new tab
- URL
- https://vibsys.put.poznan.pl/vibrations-in-physical-systems-2020-vol-31-no-3/ Opening in a new tab
- Language
- eng (en) English
- License
- Score (nominal)
- 70
- Additional fields
- Indeksowana w: Scopus
- Uniform Resource Identifier
- https://cris.pk.edu.pl/info/article/CUT7ded3381bae343ecabbb0d0d316d1406/
- URN
urn:pkr-prod:CUT7ded3381bae343ecabbb0d0d316d1406
* 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.