Design of fiber-reinforced variable-stiffness composites for different open-hole geometries with fiber continuity and curvature constraints
Source abstract
Abstract
Abstract In this study, the optimum design of fiber-reinforced composite plates with different hole geometries for various load conditions is investigated. Strain energy/compliance is optimized using three different design methodologies: constant-stiffness (CS), variable-stiffness (VS), and variable-stiffness with least-squares & continuity constraints (LSC). In all the cases, variable-stiffness and LSC designs both reveal better structural performance with reduced compliance and less stress concentrations around the hole in comparison to the optimum constant-stiffness designs. The compliance significantly decreases after optimization especially for the bi-axial loading case. Most importantly, the LSC method allows manufacturable fiber angle distributions that satisfy the maximum curvature limit, making the proposed LSC method applicable to well-established variable-stiffness manufacturing techniques such as 3-D printing and automated fiber placement. The benefits obtained by using variable-stiffness becomes less pronounced as the hole size decreases with respect to the area of the plate. The use of variable-stiffness is found to be more advantageous over shape-optimization methods of constant-stiffness composites. The comparison to the literature findings (Huang et al., 2016) reveals that 13% further reduction in structural compliance with the proposed LSC design method is possible. The proposed design method provides manufacturable variable-stiffness composites with significant improvements in structural performance.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Topology Optimization in Engineering · Mechanical Engineering and Vibrations Research
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (48)
Show source-provided references
1. Stress distribution analysis and optimization for composite laminate containing hole of different shapes10.1016/j.ast.2018.01.046 ↗
2. Analysis of GFRP stiffened composite plates with rectangular cutout10.1016/j.compstruct.2016.10.054 ↗
3. Isogeometric analysis and design of variable-stiffness aircraft panels with multiple cutouts by level set method10.1016/j.compstruct.2018.08.086 ↗
4. Pickett · 1983
5. The buckling response of carbon fibre composite panels with reinforced cut-outs10.1016/0263-8223(95)00049-6 ↗
6. Optimization of hole reinforcements by doublers10.1007/s001580050136 ↗
7. Local fibre reinforcement of holes in composite multilayered plates10.1016/j.compstruct.2011.11.017 ↗
8. Variable angle tow reinforcement design for locally reinforcing an open-hole composite plate10.1016/j.compstruct.2018.01.021 ↗
9. Design of a blade-stiffened composite panel with a hole10.1016/0263-8223(91)90033-U ↗
10. Neelakantan H, Shah D, Chan W, Neelakantan H, Shah D, Chan W. Effect of stiffener around multiple loaded holes in composite shear panel. In: 38th Structures, Structural Dynamics, and Materials Conference; 1997. p. 1369.10.2514/6.1997-1369 ↗
11. Development of a finite strip method for efficient prediction of buckling and post-buckling in composite laminates containing a cutout with/without stiffener10.1016/j.compstruct.2018.11.007 ↗
12. Shape optimization in laminated composite plates10.1016/0045-7825(89)90120-5 ↗
13. Shape optimization of interior cutouts in composite panels10.1007/BF01279653 ↗
14. On optimal shapes in materials and structures10.1007/s001580050100 ↗
15. Stress concentration analysis of fibre-reinforced multilayered composites with pin-loaded holes10.1016/j.compscitech.2006.08.018 ↗
16. Stiffness tailoring for improved compressive strength of composite plates with holes10.2514/3.9853 ↗
17. Using multicriterion optimization for strength design of composite laminates10.1016/j.compstruct.2003.09.032 ↗
18. Application of genetic algorithms to stiffness optimization of laminated composite plates with stress-concentrated open holes
19. Postbuckling analysis with progressive damage modeling in tailored laminated plates and shells with a cutout10.1016/S0263-8223(02)00233-7 ↗
20. Maximization of buckling load of laminated composite plates with central circular holes using MFD method10.1007/s00158-007-0119-1 ↗
21. Stacking sequence optimization for maximum strengths of laminated composite plates using genetic algorithm and isogeometric analysis10.1016/j.compstruct.2014.05.011 ↗
22. Es-pim applied to buckling of variable angle tow laminates10.1016/j.compstruct.2018.10.058 ↗
23. Buckling optimization of composite cylinders for axial compression: a design methodology considering a variable-axial fiber layout10.1016/j.compstruct.2019.110928 ↗
24. Cross-section optimization of topologically-optimized variable-axial anisotropic composite structures
25. Automated fiber placement head for manufacturing of innovative aerospace stiffening structures
26. On manufacturing constraints for tow-steered composite design optimization10.1016/j.compstruct.2018.07.100 ↗
27. Manufacturing characteristics of the continuous tow shearing method for manufacturing of variable angle tow composites10.1016/j.compositesa.2014.02.019 ↗
28. Waviness and fiber volume content analysis in continuous carbon fiber reinforced plastics made by tailored fiber placement10.1016/j.compstruct.2019.110910 ↗
29. In-plane response of laminates with spatially varying fiber orientations-variable stiffness concept10.2514/3.11613 ↗
30. Composites: Part B multi-objective optimization of curvilinear fiber shapes for laminated composite plates by using NSGA-II10.1016/j.compositesb.2012.07.056 ↗
31. Framework for the buckling optimization of variable-angle tow composite plates10.2514/1.J054029 ↗
32. On the effective integration of manufacturability constraints within the multi-scale methodology for designing variable angle-tow laminates10.1016/j.compstruct.2016.11.018 ↗
33. Design of variable stiffness composite structures using lamination parameters with fiber steering constraint10.1016/j.compositesb.2019.02.004 ↗
34. The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes10.1016/0263-8223(91)90035-W ↗
35. Tailoring for strength of composite steered-fibre panels with cutouts10.1016/j.compositesa.2010.08.011 ↗
36. Stacking sequence optimisation of variable stiffness laminates with manufacturing constraints10.1016/j.compstruct.2015.02.044 ↗
37. Buckling optimization of variable-stiffness composite panels based on flow field function10.1016/j.compstruct.2017.08.081 ↗
38. Optimizing fiber direction in perforated orthotropic media to reduce stress concentration10.1177/0021998308103608 ↗
39. Strength improvement by fibre steering around a pin loaded hole10.1016/S0263-8223(02)00105-8 ↗
40. Design of composite structures reinforced curvilinear fibres using FEM10.1016/j.compositesa.2016.04.005 ↗
41. Design of variable stiffness panels for maximum strength using lamination parameters10.1016/j.compositesb.2010.11.005 ↗
42. Fiber path optimization based on a family of curves in composite laminate with a center hole10.1016/j.compositesb.2016.11.051 ↗
43. Tensile properties of variable stiffness composite laminates with circular holes based on potential flow functions10.1007/s00419-016-1126-8 ↗
44. An efficient reanalysis assisted optimization for variable-stiffness composite design by using path functions10.1016/j.compstruct.2016.06.043 ↗
45. Parametrization in laminate design for optimal compliance10.1016/S0020-7683(96)00023-6 ↗
46. On feasible regions of lamination parameters for lay-up optimization of laminated composites10.1098/rspa.2008.0380 ↗
47. ASTM. Standard test method for open-hole tensile strength of polymer matrix composite laminates; 2018. pp. 1–7.
48. Curvilinear variable stiffness 3D printing technology for improved open-hole tensile strength