Details
| Originalsprache | Englisch |
|---|---|
| Seiten (von - bis) | 1865-1876 |
| Seitenumfang | 12 |
| Fachzeitschrift | Composite structures |
| Jahrgang | 92 |
| Ausgabenummer | 8 |
| Publikationsstatus | Elektronisch veröffentlicht (E-Pub) - 28 Jan. 2010 |
| Extern publiziert | Ja |
Abstract
The dynamic response of angle-ply laminated composite plates traversed by a moving mass or a moving force is investigated. For this purpose, a finite element method based on the first-order shear deformation theory is used. Stationary and adaptive mesh techniques have been applied as two different meshing schemes. The adaptive mesh strategy is then used to avoid off-nodal position of moving mass. In this manner, the finite element mesh is continuously adapted to follow and comply with the path of moving mass. A Newmark direct integration method is employed to solve the equations of motion. Parametric study is directed to find out how different parameters like mass of the moving object as well as the type of the angle-ply laminated composite plates affect the dynamic response. Numerical results show the significant effects of the stacking order on the dynamic responses of the composite structures under a moving mass. It is found that although [30/-60/-60/30] lamination shows the highest maximum vertical deflection but [-45/45/45/-45] lamination has the highest value of the dynamic amplification factor. The dynamic amplification factor for different stacking orders and mass velocities is less than 1.25.
ASJC Scopus Sachgebiete
- Werkstoffwissenschaften (insg.)
- Keramische und Verbundwerkstoffe
- Ingenieurwesen (insg.)
- Tief- und Ingenieurbau
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in: Composite structures, Jahrgang 92, Nr. 8, 28.01.2010, S. 1865-1876.
Publikation: Beitrag in Fachzeitschrift › Artikel › Forschung › Peer-Review
}
TY - JOUR
T1 - Dynamic analysis of laminated composite plates traversed by a moving mass based on a first-order theory
AU - Ghafoori, E.
AU - Asghari, M.
PY - 2010/1/28
Y1 - 2010/1/28
N2 - The dynamic response of angle-ply laminated composite plates traversed by a moving mass or a moving force is investigated. For this purpose, a finite element method based on the first-order shear deformation theory is used. Stationary and adaptive mesh techniques have been applied as two different meshing schemes. The adaptive mesh strategy is then used to avoid off-nodal position of moving mass. In this manner, the finite element mesh is continuously adapted to follow and comply with the path of moving mass. A Newmark direct integration method is employed to solve the equations of motion. Parametric study is directed to find out how different parameters like mass of the moving object as well as the type of the angle-ply laminated composite plates affect the dynamic response. Numerical results show the significant effects of the stacking order on the dynamic responses of the composite structures under a moving mass. It is found that although [30/-60/-60/30] lamination shows the highest maximum vertical deflection but [-45/45/45/-45] lamination has the highest value of the dynamic amplification factor. The dynamic amplification factor for different stacking orders and mass velocities is less than 1.25.
AB - The dynamic response of angle-ply laminated composite plates traversed by a moving mass or a moving force is investigated. For this purpose, a finite element method based on the first-order shear deformation theory is used. Stationary and adaptive mesh techniques have been applied as two different meshing schemes. The adaptive mesh strategy is then used to avoid off-nodal position of moving mass. In this manner, the finite element mesh is continuously adapted to follow and comply with the path of moving mass. A Newmark direct integration method is employed to solve the equations of motion. Parametric study is directed to find out how different parameters like mass of the moving object as well as the type of the angle-ply laminated composite plates affect the dynamic response. Numerical results show the significant effects of the stacking order on the dynamic responses of the composite structures under a moving mass. It is found that although [30/-60/-60/30] lamination shows the highest maximum vertical deflection but [-45/45/45/-45] lamination has the highest value of the dynamic amplification factor. The dynamic amplification factor for different stacking orders and mass velocities is less than 1.25.
KW - Composite plate
KW - Dynamic response
KW - Finite element method
KW - Moving force
KW - Moving mass
KW - Shear deformation
UR - http://www.scopus.com/inward/record.url?scp=77950371124&partnerID=8YFLogxK
U2 - 10.1016/j.compstruct.2010.01.011
DO - 10.1016/j.compstruct.2010.01.011
M3 - Article
AN - SCOPUS:77950371124
VL - 92
SP - 1865
EP - 1876
JO - Composite structures
JF - Composite structures
SN - 0263-8223
IS - 8
ER -