Tensile Failure Strength Analysis and Experimental Confirmation of Stitch Reinforced Composite of T-stiffened Structure
Source abstract
Abstract
Based on the progressive failure analysis method, taking account of 7 kinds of failure modes: stitch thread failure mode, resin extend (or compress) failure mode, fibre extend (or compress) failure mode, extend (or compress) delamination failure mode, a new failure analysis FE model was proposed for predicting the tensile strength of stitch-reinforced composite T-stiffened structures. The 3D solid element and truss element were used to simulate laminate and stitch thread individually in the FE model. The Hashin failure criterion and stiffness degradation technology are used to analyze damage failure of the stitch T-stiffened structure. Comparing the initial and final damage failure strength with those of experiments on stitch composite T-stiffened structures validated the Python secondary development program for the FE model presented in the paper. There was good agreement between the failure strength from the damage failure analysis and that of the experiment. This indicated that the model was correct, and that it could be a reference for stitch-reinforced composite design and analysis.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Mechanical Behavior of Composites · Structural Analysis and Optimization · Structural Load-Bearing Analysis
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Beijing Aeronautical Manufacturing Technology Research Institute, Beijing 100024, P R China
References (15)
Show source-provided references
1. 10.1016/S0263-8223(02)00058-210.1016/S0263-8223(02)00058-2 ↗
2. Shaojie Chen · The aviation manufacturing technique · 2005 · 34
3. 10.1016/j.compstruct.2006.06.02510.1016/j.compstruct.2006.06.025 ↗
4. Freitas G. · Journal of Advanced Materials · 1994 · 25 · 36
5. 10.1016/S1359-835X(04)00180-010.1016/S1359-835X(04)00180-0 ↗
6. Glaessgen E.H. · Delamination and stitch failure in stitched composite joints
7. 10.1016/S0266-3538(03)00217-310.1016/S0266-3538(03)00217-3 ↗
8. 10.1016/S0266-3538(03)00223-910.1016/S0266-3538(03)00223-9 ↗
9. 10.1016/S0266-3538(96)00143-110.1016/S0266-3538(96)00143-1 ↗
10. 10.1177/002199830203600854910.1177/0021998302036008549 ↗
11. 10.1177/002199830303474110.1177/0021998303034741 ↗
12. Ying Yan · Acta Aeronautica et Astronautica Sinica · 2004 · 25 · 267
13. Ying Yan · Acta Materiae Compositae Sinica · 2004 · 21 · 179
14. 10.1115/1.315366410.1115/1.3153664 ↗
15. Hibbitt Karlsson · 2004