A novel synergistic multi-scale modeling framework to predict micro- and meso-scale damage behaviors of 2D triaxially braided composite
Source abstract
Abstract
A novel synergistic multi-scale modeling framework with a coupling of micro- and meso-scale is proposed to predict damage behaviors of 2D-triaxially braided composite (2DTBC). Based on the Bridge model, the internal stress and micro damage of constituent materials are respectively coupled with the stress and damage of tow. The initial effective elastic properties of tow (IEEP) used as the predefined data are estimated by micro-mechanics models. Due to in-situ effects, stress concentration factor (SCF) is considered in the micro matrix, exhibiting progressive damage accumulation. Comparisons of IEEP and strengths between the Bridge and Chamis’ theory are conducted to validate the values of IEEP and SCF. Based on the representative volume element (RVE), the macro properties and damage modes of 2DTBC are predicted to be consistent with available experiments and meso-scale simulation. Both axial and transverse damage mechanisms of 2DTBC under tensile or compressive load are revealed. Micro fiber and matrix damage accumulations have significant effects on the meso-scale axial and transverse damage of tows due to multi-scale coupling effects. Different from existing meso-/multi-scale models, the proposed multi-scale model can capture a crucial phenomenon that the transverse damage of tow is vulnerable to micro fiber fracture. The proposed multi-scale framework provides a robust tool for future systematic studies on constituent materials level to larger-scale aeronautical materials.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Mechanical Behavior of Composites · Composite Material Mechanics · Fiber-reinforced polymer composites
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
State Key Laboratory of Advanced Design and Manufacturing for Vehicle Body, Hunan University, Changsha, Hunan, China
College of Mechanical and Vehicle Engineering, Hunan University, Changsha, Hunan, China
Funding
Hunan Provincial Innovation Foundation for Postgraduate · China Scholarship Council · Foundation for Innovative Research Groups of the National Natural Science Foundation of China · National Natural Science Foundation of China
References (71)
Show source-provided references
1. 10.1016/j.compstruct.2019.11096610.1016/j.compstruct.2019.110966 ↗
2. 10.1016/0266-3538(96)00005-X10.1016/0266-3538(96)00005-X ↗
3. 10.1061/(ASCE)EM.1943-7889.000018110.1061/(ASCE)EM.1943-7889.0000181 ↗
4. Camanho PP, Davila CG (2002) Mixed-mode decohesion finite elements for the simulation of delamination in composite materials. NASA/TM-2002–211737, pp.1–37.
5. 10.1177/105678951985450610.1177/1056789519854506 ↗
6. Chamis CC (1984) Mechanics of composite materials-past, present and future. Journal of Composites Technology and Research 11(1): 3–14.10.1520/CTR10143J ↗
7. Cheng J (2006) Material modeling of strain rate dependent polymer and 2D triaxially braided composites. PhD Dissertation, University of Akron, Akron, OH.
8. Dassault Systemes (2013) Abaqus 6.13: Analysis User's Manual .
9. 10.1016/j.compscitech.2019.10769110.1016/j.compscitech.2019.107691 ↗
10. 10.1016/j.compstruct.2008.07.01610.1016/j.compstruct.2008.07.016 ↗
11. 10.1061/(ASCE)AS.1943-5525.000013510.1061/(ASCE)AS.1943-5525.0000135 ↗
12. 10.1016/j.compscitech.2018.12.00310.1016/j.compscitech.2018.12.003 ↗
13. 10.1016/j.compstruct.2018.01.02410.1016/j.compstruct.2018.01.024 ↗
14. 10.1016/j.compstruct.2018.10.01710.1016/j.compstruct.2018.10.017 ↗
15. 10.1016/S0167-577X(99)00069-510.1016/S0167-577X(99)00069-5 ↗
16. 10.1177/08927057000130040110.1177/089270570001300401 ↗
17. 10.1016/S0266-3538(99)00148-710.1016/S0266-3538(99)00148-7 ↗
18. 10.1016/S1359-835X(00)00142-110.1016/S1359-835X(00)00142-1 ↗
19. 10.1016/S0266-3538(03)00220-310.1016/S0266-3538(03)00220-3 ↗
20. Huang ZM (2018) Failure and Strength of Composite Materials. Science Press, Beijing, 95–103. (in Chinese)
21. 10.1016/S0263-8223(02)00047-810.1016/S0263-8223(02)00047-8 ↗
22. 10.1016/j.compstruct.2017.11.04610.1016/j.compstruct.2017.11.046 ↗
23. 10.1177/002199831246026110.1177/0021998312460261 ↗
24. 10.1016/j.ijmecsci.2013.08.01010.1016/j.ijmecsci.2013.08.010 ↗
25. 10.1142/S175882511650034410.1142/S1758825116500344 ↗
26. 10.1016/j.compscitech.2021.10866410.1016/j.compscitech.2021.108664 ↗
27. 10.1016/j.ijmecsci.2019.10530710.1016/j.ijmecsci.2019.105307 ↗
28. 10.1016/j.tws.2018.08.02210.1016/j.tws.2018.08.022 ↗
29. 10.1007/s10853-018-2248-x10.1007/s10853-018-2248-x ↗
30. 10.1016/j.ijmecsci.2019.03.02810.1016/j.ijmecsci.2019.03.028 ↗
31. 10.1007/s10853-018-2928-610.1007/s10853-018-2928-6 ↗
32. 10.1177/002199830809390910.1177/0021998308093909 ↗
33. Johnson ER (2002) Analysis for the progressive failure response of textile composite fuselage frames. Technical Report NASA/NAG-1–01123.
34. 10.1177/002199831244988610.1177/0021998312449886 ↗
35. 10.1177/002199831349947710.1177/0021998313499477 ↗
36. Kelkar AD, Whitcomb JD (2009) Characterization and structural behavior of braided composites. Technical Report FAA: DOT/FAA/AR-08/52.
37. 10.1016/j.compositesa.2007.01.01710.1016/j.compositesa.2007.01.017 ↗
38. Li X, Binienda WK, Goldberg RK (2010) Finite element model for failure study of two dimensional triaxially braided composite. NASA/TM-2010-216372.10.1061/41096(366)83 ↗
39. 10.1061/(ASCE)AS.1943-5525.000002910.1061/(ASCE)AS.1943-5525.0000029 ↗
40. 10.1016/j.tws.2018.07.04710.1016/j.tws.2018.07.047 ↗
41. Littell JD (2008) The experimental and analytical characterization of the macromechanical response for triaxially braided composite. PhD Dissertation, University of Akron, Akron, OH.
42. 10.1016/j.compositesa.2009.08.00110.1016/j.compositesa.2009.08.001 ↗
43. 10.1177/002199831246923710.1177/0021998312469237 ↗
44. 10.1061/(ASCE)AS.1943-5525.000056010.1061/(ASCE)AS.1943-5525.0000560 ↗
45. 10.1061/9780784479179.05310.1061/9780784479179.053 ↗
46. Perez J, Johnson E, Boitnott R (2013) Tests of braided composite fuselage frames under radial inward load. In : 41st Structures, Structural Dynamics, Materials Conference Exhibit . Available at: https://arc.aiaa.org/doi/10.2514/6.2000-1547 (accessed 8 July 2021).
47. 10.1016/j.compscitech.2006.01.02210.1016/j.compscitech.2006.01.022 ↗
48. 10.1016/j.ijmecsci.2019.04.02410.1016/j.ijmecsci.2019.04.024 ↗
49. 10.1007/s10443-017-9623-710.1007/s10443-017-9623-7 ↗
50. 10.1016/S0266-3538(98)00078-510.1016/S0266-3538(98)00078-5 ↗
51. 10.1016/j.compstruc.2010.12.00310.1016/j.compstruc.2010.12.003 ↗
52. 10.1016/j.compscitech.2006.01.02610.1016/j.compscitech.2006.01.026 ↗
53. 10.1016/j.ijimpeng.2017.08.00210.1016/j.ijimpeng.2017.08.002 ↗
54. 10.1177/00219983710050010610.1177/002199837100500106 ↗
55. 10.1016/j.compositesb.2019.03.02710.1016/j.compositesb.2019.03.027 ↗
56. 10.1016/j.compstruct.2017.07.02310.1016/j.compstruct.2017.07.023 ↗
57. 10.1007/s10853-016-9901-z10.1007/s10853-016-9901-z ↗
58. 10.1177/105678952092707410.1177/1056789520927074 ↗
59. 10.1177/105678951666361310.1177/1056789516663613 ↗
60. 10.1007/s10443-014-9386-310.1007/s10443-014-9386-3 ↗
61. 10.1016/j.mechmat.2014.05.00210.1016/j.mechmat.2014.05.002 ↗
62. 10.1016/j.compositesa.2013.11.00910.1016/j.compositesa.2013.11.009 ↗
63. 10.1061/(ASCE)AS.1943-5525.000036910.1061/(ASCE)AS.1943-5525.0000369 ↗
64. 10.1016/j.compstruct.2015.01.03410.1016/j.compstruct.2015.01.034 ↗
65. 10.1007/s10443-016-9579-z10.1007/s10443-016-9579-z ↗
66. 10.1177/105678951990078410.1177/1056789519900784 ↗
67. 10.1007/s10443-018-9732-y10.1007/s10443-018-9732-y ↗
68. 10.1016/j.compositesa.2018.04.02010.1016/j.compositesa.2018.04.020 ↗
69. 10.1016/j.compscitech.2019.01.00810.1016/j.compscitech.2019.01.008 ↗
70. 10.1177/002199830809455110.1177/0021998308094551 ↗
71. 10.1016/j.compositesb.2012.10.02610.1016/j.compositesb.2012.10.026 ↗