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Vibration and damping of laminated, composite-material plates including thickness-shear effects
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Siu, C. C. Bert, C. W. |
| Copyright Year | 1972 |
| Description | An analytical investigation of sinusoidally forced vibration of laminated, anisotropic plates including bending-stretching coupling, thickness-shear flexibility, all three types of inertia effects, and material damping is presented. In the analysis the effects of thickness-shear deformation are considered by the use of a shear correction factor K, analogous to that used by Mindlin for homogeneous plates. Two entirely different approaches for calculating the thickness-shear factor for a laminate are presented. Numerical examples indicate that the value of K depends on the layer properties and the stacking sequence of the laminate. |
| File Size | 6522331 |
| Page Count | 259 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720022240 |
| Archival Resource Key | ark:/13960/t4km42c6j |
| Language | English |
| Publisher Date | 1972-03-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Dynamic Structural Analysis Stress Analysis Composite Materials Numerical Analysis Deformation Shear Stress Vibration Effects Laminates Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
