Abstract
The response of composite laminated plates subjected to non-stationary random excitation is determined. First-order shear deformation theory is used for the analysis of symmetric cross-ply and antisymmetric angle-ply plates. The time-dependent component of the forcing function is taken as a product of a well-defined, slowly varying envelope function, and a noise function, assumed to be white or narrow-band random excitation.
Original language | English |
---|---|
Pages (from-to) | 99-113 |
Number of pages | 15 |
Journal | Structural Safety |
Volume | 6 |
Issue number | 2-4 |
DOIs | |
State | Published - 1 Jan 1989 |
Externally published | Yes |
Keywords
- composite materials
- first-order shear deformation theory
- random vibration
ASJC Scopus subject areas
- Civil and Structural Engineering
- Building and Construction
- Safety, Risk, Reliability and Quality