Abstract
In order to analyze tear strength of laminated envelope reinforced by Kevlar-plain woven fabric, a new physical model is developed to calculate the initial single edge notched (SEN) shape. The arithmetical displacement method is proposed to calculate the stress distribution of the crack tip. Then three types of specimens are tested. It is found that the tear strength between the physical model and experiment tests is approximate, and the deviation is lower than 5%. When compared with the stress intensity factor, this model is more accurate and suitable, and the initial crack length ratio could even reach 0.60.
| Original language | English |
|---|---|
| Pages (from-to) | 21-30 |
| Number of pages | 10 |
| Journal | Engineering Fracture Mechanics |
| Volume | 127 |
| DOIs | |
| State | Published - Sep 2014 |
Keywords
- Computational modeling
- Laminated structures
- Stress intensity factor
- Tear strength
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