Abstract
An improved model to predict the strength of a composite laminate containing a slit notch through crack is developed, assuming the material characteristic dimension to be an exponential function of crack size. A superposition method is developed which allows data for all composite material systems described by the developed model to be superimposed. A generalized notch sensitivity factor is introduced which allows quantitative characterization of the notch sensitivity of a given material with respect to a reference notch-insensitive material.
| Original language | English |
|---|---|
| Pages (from-to) | 247-253 |
| Number of pages | 7 |
| Journal | Materials science and engineering |
| Volume | 45 |
| Issue number | 3 |
| DOIs | |
| State | Published - 1980 |
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