Abstract
By viewing a composite lamina as a homogeneous solid whose directional strengths are random variables, lamina reliability under multiaxial stresses may be determined using either an interactive or a noninteractive criterion. From the reliability values for the individual laminae comprising a given laminate, the authors have previously proposed a method for determining bounds for the overall laminate reliability. In this paper, simple physically plausible phenomenological rules arc proposed for redistribution of load after a lamina has failed within the confines of a laminate. These rules arc illustrated by application to [0/±15], and [90/±45/0], graphite/epoxy (GR/EP) laminates and the results are compared to the previously proposed bounds.
| Original language | English |
|---|---|
| Pages (from-to) | 1459-1475 |
| Number of pages | 17 |
| Journal | Journal of Composite Materials |
| Volume | 25 |
| Issue number | 11 |
| DOIs | |
| State | Published - Nov 1991 |
Fingerprint
Dive into the research topics of 'Reliability Analysis of Composite Laminates with Load Sharing'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver