Off-axis crack-coupled failure model and mechanical properties of flexible composite materials
Source abstract
Abstract
Fiber-reinforced flexible composites are critical materials for stratospheric airship envelopes owing to their excellent mechanical properties and weather resistance. To address the challenge of coupled off-axis and crack-induced failures throughout the entire manufacturing-service cycle, this study overcomes the traditional research limitation of treating “damage-free off-axis strength prediction” and “single-angle tear strength analysis” as separate issues. Based on the Tsai–Hill failure criterion, we propose a synergistic theoretical framework that incorporates dual parameters: off-axis angle and crack length. By introducing an off-axis angle factor and integrating a single-angle failure model, a new failure model that couples multiple damage mechanisms was developed. Uniaxial tensile tests were conducted systematically under varying off-axis angles and crack lengths, and the results demonstrate that the proposed model provides high prediction accuracy and reliability.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Aerospace Engineering and Energy Systems · Structural Analysis and Optimization · Mechanical Behavior of Composites
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
School of Mechanical and Electrical Engineering, Henan Institute of Science and Technology 1 , Xinxiang 453003,
Zhengzhou Foguang Electric Power Equipment Co., Ltd. 2 , Zhengzhou 450001,
School of Mechanical and Power Engineering, Henan Polytechnic University 3 , Jiaozuo 454003,
Funding
Natural Science Foundation of Henan Province · National Natural Science Foundation of China · Henan Provincial Science and Technology Research Project
References (33)
Show source-provided references
1. Stratospheric airship trajectory planning in wind field using deep reinforcement learning10.1016/j.asr.2024.08.057 ↗
2. Hierarchical reinforcement learning method for long-horizon path planning of stratospheric airship10.1016/j.ast.2025.110075 ↗
3. Mechanical and gas barrier properties of naturally and artificially weathered high-performance fiber reinforced laminated structures for stratospheric airship envelope10.1007/s12221-025-00961-w ↗
4. Meso-scale tearing mechanism analysis of flexible fabric composite for stratospheric airship via experiment and numerical simulation10.1007/s12204-022-2431-8 ↗
5. Tear strength of a laminated fabric for stratospheric airship under uniaxial and biaxial tests10.1177/15589250211001822 ↗
6. Failure properties of flexible composite under trouser-shaped tests10.1177/00219983221089714 ↗
7. Mechanical properties of the surface membrane of lattice spacer-fabric flexible inflatable composites10.1177/00405175211046623 ↗
8. Effects of on-axis and off-axis tension on uniaxial mechanical properties of plain woven fabrics for inflated structures10.1016/j.compstruct.2017.02.009 ↗
9. Mechanical behaviors and elastic parameters of laminated fabric URETEK3216LV subjected to uniaxial and biaxial loading10.1007/s10443-016-9576-2 ↗
10. Full-strain range characteristics of the Poisson’s ratio for coated biaxial warp-knitted fabrics under bias tensile loading10.1177/0040517518783359 ↗
11. Mechanical properties and strength criteria of fabric membrane for the stratospheric airship envelope10.1007/s10443-016-9515-2 ↗
12. Characterizing the macroscopic response and local deformation mechanisms of a unidirectional non-crimp fabric10.1016/j.compositesa.2022.106857 ↗
13. A 2-D fabric anisotropic hyperelastic constitutive model based on micromechanics analysis10.1016/j.ijmecsci.2024.109560 ↗
14. On the biaxial testing and strength of coated fabrics: Paper demonstrates that improved specimens allow the measurement of the true biaxial breaking strength10.1007/bf02328607 ↗
15. Biaxial strength determination of woven fabric composite for airship structural envelope based on novel specimens10.1016/j.compstruct.2017.10.067 ↗
16. Biaxial constitutive relationship and strength criterion of composite fabric for airship structures10.1016/j.compstruct.2019.02.028 ↗
17. Large-strain hyperelastic constitutive model of envelope material under biaxial tension with different stress ratios10.3390/ma11091780 ↗
18. Application of composite fracture models to coated fabrics10.1177/152808379402400205 ↗
19. Central crack tearing test and fracture parameter determination of PTFE coated fabric10.1016/j.conbuildmat.2019.03.046 ↗
20. Tearing analysis for textile reinforced soft composites under mono-axial and bi-axial tensile stresses10.1016/s0263-8223(03)00099-0 ↗
21. Comparisons of trapezoid tearing behaviors of uncoated and coated woven fabrics from experimental and finite element analysis10.1177/1056789512450524 ↗
22. Static tearing, part II: Analysis of stages of static tearing in cotton fabrics for wing-shaped test specimens10.1177/0040517507081310 ↗
23. A comparative analysis of tear strength methods10.1016/j.dyepig.2003.10.008 ↗
24. Mechanics of elastic performance of textile materials: Part XII: Relation of certain geometric factors to the tear strength of woven fabrics10.1177/004051755502501003 ↗
25. Modified stress field model for critical tearing strength of architectural coated fabrics10.1177/15280837221106232 ↗
26. Tearing analysis of PVC coated fabric under uniaxial and biaxial central tearing tests10.1177/1528083720934513 ↗
27. Central tearing behavior of PVDF coated fabrics with multiple initial notches10.1002/pc.25885 ↗
28. Central tearing behaviors of PVC coated fabrics with initial notch10.1016/j.compstruct.2018.09.104 ↗
29. Tear propagation behavior with a novel analytical model on envelope material10.1088/2053-1591/ab381f ↗
30. Tearing behaviors of flexible fiber-reinforced composites for the stratospheric airship envelope10.1007/s10443-016-9539-7 ↗
31. Nonlinear mechanical response and residual tearing strength of flexible composite sheet with single edge-crack under uniaxial tension10.1016/j.engfracmech.2021.108056 ↗
32. Experimental study on uniaxial and biaxial tensile properties of coated fabric for airship envelopes10.1177/0731684413515540 ↗
33. Evaluation of bias-extension and picture-frame test methods for the measurement of intraply shear properties of PP/glass commingled fabrics10.1016/s0263-8223(03)00057-6 ↗