Response surface analysis of biaxial mechanical properties and elastic parameters for woven fabric composites
Source abstract
Abstract
This paper describes a self-developed MATLAB program for achieving complex deformation properties and accurate elastic parameters of woven fabrics. Using this program, the response surface analyses of deformation and elastic parameters were conducted to reveal the variation and evolution in stiffness, Poisson’s ratio, and orthotropy of the laminated woven fabric composite under different loading/unloading stages, cycles, stress levels and ratios, which is a further development of our prior work. Results show that elastic parameters and orthotropic characteristics of the material vary noticeably with the loading/unloading stages, cycles, stress levels, and ratios. As higher values are required to model the remarkable warp–weft interaction and large negative strains, Poisson’s ratios in boundary regions with a maximum of 1.0 (loading) or 1.5 (unloading) are outside the bounds normally expected for these parameters. In addition, the proposed method is feasible to evaluate elastic parameters for any stress state, and thereby provides new insights into underlying deformation mechanisms of woven fabric composites.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Structural Analysis and Optimization · Textile materials and evaluations · Mechanical Behavior of Composites
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
School of Science, Nanjing University of Science and Technology, Nanjing, China
Space Structures Research Center, Shanghai Jiao Tong University, Shanghai, China
School of Mechanical Engineering, Nanjing University of Science and Technology, Nanjing, China
Funding
undamental Research Funds for the Central Universities · China Postdoctoral Science Foundation · National Natural Science Foundation of China · Fundamental Research Program of Jiangsu Province
References (44)
Show source-provided references
1. Nayler A. Airship activity and development world-wide-2003. In: AIAA’s 3rd aviation technology, integration and operations (ATIO) technical forum , Denver, USA, 17–19 November 2003, pp.6727–6737. USA: AIAA.10.2514/6.2003-6727 ↗
2. Gan X · 2005
3. 10.1016/j.compstruct.2006.04.06010.1016/j.compstruct.2006.04.060 ↗
4. 10.5139/IJASS.2012.13.2.17010.5139/IJASS.2012.13.2.170 ↗
5. Komatsu K, Sano MA and Kakuta Y. Development of high-specific-strength envelope materials. In: AIAA’s 3rd aviation technology, integration and operations (ATIO) technical forum , Denver, USA, 17–19 November 2003, pp.6765–6777. AIAA.10.2514/6.2003-6765 ↗
6. 10.1177/073168441351554010.1177/0731684413515540 ↗
7. 10.1177/073168441665294710.1177/0731684416652947 ↗
8. 10.1177/073168441245989810.1177/0731684412459898 ↗
9. 10.1061/(ASCE)MT.1943-5533.000127310.1061/(ASCE)MT.1943-5533.0001273 ↗
10. 10.1061/(ASCE)MT.1943-5533.000126510.1061/(ASCE)MT.1943-5533.0001265 ↗
11. 10.1016/j.conbuildmat.2015.01.07410.1016/j.conbuildmat.2015.01.074 ↗
12. Forster B · 2004
13. MSAJ/M-02:1995. Standard of membrane structures.
14. DG/TJ08-2019:2007. Technical specification for inspection of membrane structures.
15. Uhlemann J, Stranghoner N, Schmidt H, et al. Effects on elastic constants of technical membranes applying the evaluation methods of MSAJ/M-02-1995. In: The v international conference on textile composites and inflatable structures , Barcelona, 5–7 October 2011, pp. 450–458. Barcelona: Structural Membranes.
16. Galliot C and Luchsinger RH. Determination of the response of coated fabrics under biaxial stress: comparison between different test procedures. In: The v international conference on textile composites and inflatable structures , Barcelona, 5–7 October 2011, pp.651–660. Barcelona: Structural Membranes.
17. 10.1016/j.compstruct.2009.04.01610.1016/j.compstruct.2009.04.016 ↗
18. 10.1016/j.compstruc.2003.07.00510.1016/j.compstruc.2003.07.005 ↗
19. 10.1177/15280837000300020410.1177/152808370003000204 ↗
20. Blum R and Bogner B. Evaluation method for the elastic moduli, www.tensinet.com/files/TensiNetPublications/TensiNews3_2002_09-1.pdf(2014, accessed 3 May 2015).
21. Day AS. Stress strain equations for non-linear behavior of coated woven fabrics. In: IASS symposium proceedings: shells, membranes and space frames , Osaka, Japan, 12–15 September 1986, pp.120–124. IASS.
22. Testa RB · J Eng Mech ASCE · 1978 · 104 · 1027
23. Bridgens BN · Struct Eng · 2004 · 82 · 21
24. 10.1080/00405000.2011.60282410.1080/00405000.2011.602824 ↗
25. 10.4188/jte.52.18910.4188/jte.52.189 ↗
26. 10.1016/S0141-0296(98)00024-810.1016/S0141-0296(98)00024-8 ↗
27. 10.1016/j.engstruct.2006.09.00110.1016/j.engstruct.2006.09.001 ↗
28. 10.1016/j.ijsolstr.2004.10.03010.1016/j.ijsolstr.2004.10.030 ↗
29. 10.1016/j.conbuildmat.2013.08.06010.1016/j.conbuildmat.2013.08.060 ↗
30. 10.1177/073168441348150910.1177/0731684413481509 ↗
31. Chen J · Appl Compos Mater · 2017
32. 10.1260/02663510878695987010.1260/026635108786959870 ↗
33. 10.1177/004051751349425910.1177/0040517513494259 ↗
34. 10.1177/073168441351270510.1177/0731684413512705 ↗
35. 10.1177/073168441350285810.1177/0731684413502858 ↗
36. Liu L · Mater Res Innov · 2015 · 19 · 606
37. BS EN ISO 139-2005:2005. Textiles – standard atmospheres for conditioning and testing.
38. 10.1016/j.ijsolstr.2011.03.00910.1016/j.ijsolstr.2011.03.009 ↗
39. 10.1016/j.compscitech.2012.10.01210.1016/j.compscitech.2012.10.012 ↗
40. 10.1177/00219980177266138010.1177/002199801772661380 ↗
41. Chen J · J Donghua Univ · 2015 · 32 · 351
42. 10.1016/j.compstruct.2004.05.01710.1016/j.compstruct.2004.05.017 ↗
43. 10.1016/j.compositesa.2014.07.01510.1016/j.compositesa.2014.07.015 ↗
44. 10.1177/152808371667915710.1177/1528083716679157 ↗