A novel continuum damage evolution model based on the concept of damage driving force for unidirectional composites
Source abstract
Abstract
A novel damage evolution model for unidirectional (UD) composites is established in this paper in the context of continuum damage mechanics (CDM). It addresses matrix cracking and it is to be applied along with the damage representation established previously. The concept of damage driving force is employed based on the Helmholtz free energy. It is shown that the damage driving force can be partitioned into three parts, resembling closely three conventional modes of fracture, respectively. A damage evolution law is derived accordingly based on the newly obtained expressions of the damage driving force. The fully rationalised Tsai-Wu criterion is employed in the model for predicting the initiation of matrix cracking damage and fibre failure, assisted with the rationalised maximum stress criterion for identifying the damage modes. A mechanism is introduced to describe the unloading behaviour as a part of the proposed model. The predictions were validated against experimental results, showing good agreement with the experiments and demonstrating the capability and effectiveness of the proposed model.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Mechanical Behavior of Composites · Structural Response to Dynamic Loads · High-Velocity Impact and Material Behavior
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Faculty of Engineering, University of Nottingham, Nottingham, UK
References (65)
Show source-provided references
1. 10.1016/j.compstruct.2017.04.01110.1016/j.compstruct.2017.04.011 ↗
2. 10.1016/B978-008043918-1/50031-910.1016/B978-008043918-1/50031-9 ↗
3. 10.1201/978131537029310.1201/9781315370293 ↗
4. 10.1111/ffe.1250210.1111/ffe.12502 ↗
5. 10.1016/j.compscitech.2020.10833510.1016/j.compscitech.2020.108335 ↗
6. 10.1016/j.engfracmech.2021.10776710.1016/j.engfracmech.2021.107767 ↗
7. 10.1016/j.euromechsol.2023.10521310.1016/j.euromechsol.2023.105213 ↗
8. 10.1177/002199831349409510.1177/0021998313494095 ↗
9. 10.1098/rspa.1945.001110.1098/rspa.1945.0011 ↗
10. 10.1016/j.compstruct.2016.10.06710.1016/j.compstruct.2016.10.067 ↗
11. 10.1002/pc.1067110.1002/pc.10671 ↗
12. 10.1016/S0266-3538(96)00139-X10.1016/S0266-3538(96)00139-X ↗
13. 10.1016/j.compstruct.2023.11714710.1016/j.compstruct.2023.117147 ↗
14. 10.1016/j.compstruct.2011.12.00210.1016/j.compstruct.2011.12.002 ↗
15. Shen H (2016) Synergistic Damage Mechanics for Multi-Directional Properties of Composite Laminates with Experimental Verification. Nanjing: Nanjing University of Aeronautics and Astronautics.
16. Haque BZ (2015) A progressive composite damage model for unidirectional and woven fabric composites. MAT162 User Manual 10. University of Delaware: Delaware, USA.
17. 10.1016/S0266-3538(02)00125-210.1016/S0266-3538(02)00125-2 ↗
18. 10.1016/S0266-3538(03)00227-610.1016/S0266-3538(03)00227-6 ↗
19. 10.1177/105678950809156310.1177/1056789508091563 ↗
20. 10.1016/S0266-3538(99)00025-110.1016/S0266-3538(99)00025-1 ↗
21. 10.1177/002199831244988710.1177/0021998312449887 ↗
22. 10.1177/002199831347871010.1177/0021998313478710 ↗
23. 10.1177/002199831349947610.1177/0021998313499476 ↗
24. 10.1177/002199831349947510.1177/0021998313499475 ↗
25. 10.1016/S0266-3538(03)00226-410.1016/S0266-3538(03)00226-4 ↗
26. Knops M (2008) Analysis of Failure in Fiber Polymer Laminates: The Theory of Alfred Puck. Berlin: Springer Science & Business Media.
27. 10.1016/j.compscitech.2005.07.04410.1016/j.compscitech.2005.07.044 ↗
28. 10.3390/jcs404015710.3390/jcs4040157 ↗
29. 10.1098/rsta.1998.027810.1098/rsta.1998.0278 ↗
30. 10.1016/j.ijmecsci.2004.12.01510.1016/j.ijmecsci.2004.12.015 ↗
31. 10.3390/jcs603008210.3390/jcs6030082 ↗
32. Li S, Xu M, Sitnikova E (2022a) Fully rationalised Tsai-Wu failure criterion for transversely isotropic materials. In: Tsai S (ed.) Double-Double – A New Perspective in Manufacture and Design of Composites. Stanford: JEC & Stanford, pp. 173–206.
33. 10.1007/s10665-021-10098-310.1007/s10665-021-10098-3 ↗
34. 10.1016/j.mtcomm.2023.10698810.1016/j.mtcomm.2023.106988 ↗
35. 10.1177/105678951878323910.1177/1056789518783239 ↗
36. LS-DYNA (2015) Keyword User’s Manual, Material Models. ANSYS: Pennsylvania, US.
37. Maplesoft (2014). Maple User Manual. Maple: Waterloo, Canada.
38. 10.1016/0167-6636(94)00053-010.1016/0167-6636(94)00053-0 ↗
39. 10.1016/j.compstruct.2014.10.00410.1016/j.compstruct.2014.10.004 ↗
40. 10.1016/j.compositesb.2014.05.01510.1016/j.compositesb.2014.05.015 ↗
41. 10.1016/j.compscitech.2019.03.02210.1016/j.compscitech.2019.03.022 ↗
42. 10.1007/978-94-007-2666-610.1007/978-94-007-2666-6 ↗
43. Ni T, Zaccariotto M, Galvanetto U (2023) A peridynamic approach to simulating fatigue crack propagation in composite materials. Philosophical Transactions. Series A, Mathematical, Physical, and Engineering Sciences 381(2240): 20210217.
44. 10.1177/105678952093962410.1177/1056789520939624 ↗
45. 10.1016/S0266-3538(01)00208-110.1016/S0266-3538(01)00208-1 ↗
46. Mathworks (2017) Matlab R2017a. Natick, MA, USA.
47. 10.1016/j.compstruct.2015.06.01210.1016/j.compstruct.2015.06.012 ↗
48. 10.1177/002199831347632810.1177/0021998313476328 ↗
49. 10.1016/j.compositesb.2017.02.03310.1016/j.compositesb.2017.02.033 ↗
50. 10.1016/S0266-3538(98)00077-310.1016/S0266-3538(98)00077-3 ↗
51. 10.1016/S0266-3538(98)00078-510.1016/S0266-3538(98)00078-5 ↗
52. 10.1016/S0266-3538(02)00093-310.1016/S0266-3538(02)00093-3 ↗
53. 10.1016/S0266-3538(03)00228-810.1016/S0266-3538(03)00228-8 ↗
54. 10.3390/ma1607288410.3390/ma16072884 ↗
55. 10.1007/s00542-018-4021-010.1007/s00542-018-4021-0 ↗
56. 10.1098/rspa.1985.005510.1098/rspa.1985.0055 ↗
57. Talreja R (1987) Internal variable damage mechanics of composite materials. Yielding, Damage, and Failure of Anisotropic Solids: 509–533.
58. 10.1017/CBO978113901606310.1017/CBO9781139016063 ↗
59. 10.1016/j.ijsolstr.2016.11.01410.1016/j.ijsolstr.2016.11.014 ↗
60. 10.1016/j.mechmat.2009.02.00910.1016/j.mechmat.2009.02.009 ↗
61. Yu T (2016) Continuum Damage Mechanics Models and Their Applications to Composite Components of Aero-Engines. Nottingham: The University of Nottingham.
62. 10.1016/j.compstruct.2015.08.10710.1016/j.compstruct.2015.08.107 ↗
63. 10.1016/S0020-7683(03)00016-710.1016/S0020-7683(03)00016-7 ↗
64. 10.1016/j.compstruct.2015.03.03010.1016/j.compstruct.2015.03.030 ↗
65. 10.1016/S0266-3538(97)00191-710.1016/S0266-3538(97)00191-7 ↗