Experimental investigation and theoretical analysis of tear propagation of GQ-6 airship envelope
Source abstract
Abstract
This paper reports the central tearing properties of a new airship envelope fabric, GQ-6, from experimental investigation and theoretical analysis. First, the effects of the load ratio, the initial crack length, and the crack orientation on the tearing mechanical properties of such material were evaluated. The experimental results revealed that the mechanical properties of GQ-6 decrease with the increase of initial crack length. Two fracture modes were observed, e.g. either along the warp or the weft yarns directions, which depend on crack orientation and load ratio. Oriented crack can be represented by non-oriented crack with crack equivalent length under biaxial condition. The toughness K IC for the fabric was determined based on experimental results, as well as critical energy release rate G IC . A comparison of the mechanical behaviors of this textile under uniaxial and biaxial tensile condition is also presented. The allowable crack length for GQ-6 envelope fabric during working condition is estimated.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Structural Analysis and Optimization · Aerospace Engineering and Energy Systems · Planetary Science and Exploration
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Space Structures Research Centre, Shanghai Jiao Tong University, Shanghai, China
References (19)
Show source-provided references
1. Khoury GA · 1999
2. Wang FX · J Ind Text · 2016 · 0 · 1
3. 10.1016/j.compstruct.2013.12.02510.1016/j.compstruct.2013.12.025 ↗
4. 10.1016/j.matdes.2015.07.13510.1016/j.matdes.2015.07.135 ↗
5. Shoji M · J Aircraft · 2008 · 5 · 1546
6. 10.1016/j.carbon.2014.05.05310.1016/j.carbon.2014.05.053 ↗
7. Meng JH · J Astronaut · 2015 · 36 · 230
8. Chen JW · Acata Materiae Compositae Sinica · 2015 · 33 · 1
9. Isida M · Int J Fract Mech · 1970 · 7 · 30110.1007/BF00184306 ↗
10. 10.1016/S0263-8223(03)00099-010.1016/S0263-8223(03)00099-0 ↗
11. 10.1016/j.compstruct.2008.11.00710.1016/j.compstruct.2008.11.007 ↗
12. Wang FX · Mater Sci Eng · 2016 · 137 · 1
13. 10.1016/0266-3538(86)90011-410.1016/0266-3538(86)90011-4 ↗
14. Chinese Aeronautical Establishment C · 1981
15. 10.1016/0013-7944(71)90043-910.1016/0013-7944(71)90043-9 ↗
16. 10.1177/15280837730030020310.1177/152808377300300203 ↗
17. 10.1177/073168441351554010.1177/0731684413515540 ↗
18. Liu DX · Adv Mater Res · 2011 · 217 · 147
19. USA DOT. FAA-P-8110-2-1995, Airship Design Criteria. 1995: 32.