Comparative study on bezier curve and linear variable angle method for variable stiffness laminates
Source abstract
Abstract
By adjusting the connection point parameter β, the Bezier curve method can make the angle of the fiber trajectory vary nonlinearly and improve the design space. In view of this, the variable‐stiffness laminates which are made by Bezier curve method and linear variable angle methods respectively are used as the research objects. Under the same conditions, taking the stacking sequence of (0 ± <20[β]60>)2s as an example, the influences of the number and the curvature of tows on these two kinds of variable angle trajectory are discussed. Meanwhile, the buckling behaviors of these two kinds of variable angle laminates are comparatively analyzed. The results show when the connection point parameter β is 0.6, the trajectory and curvature change of Bezier curve method is consistent with the linear variable angle method. For the number of tow in the same area, the number of Bezier curve is less than that of linear variable angle method when the connection point parameter β is >0.6. Furthermore, for the Bezier curve method, the buckling load is first decreased and then increased with the increase of connection point parameter β. While the connection point parameter β is over 0.6, the buckling load of Bezier curve method is better than that of linear variable angle method. POLYM. COMPOS., 40:952–960, 2019. © 2018 Society of Plastics Engineers
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Research context
OpenAlex topics: Mechanical Engineering and Vibrations Research · Composite Structure Analysis and Optimization · Dynamics and Control of Mechanical Systems
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Department of Mechanical Manufacturing and Automation Harbin Institute of Technology Harbin 150001 China
Department of Mechanical Manufacturing and Automation Qiqihar University Qiqihar 161001 China
Funding
National Natural Science Foundation of China
References (29)
Show source-provided references
1. 10.1016/j.ijsolstr.2016.06.00710.1016/j.ijsolstr.2016.06.007 ↗
2. http://composites.usc.edu/projects/automated-defect-evaluation-software-for-ultrasonic-ndi.htm.2017‐05‐1.
3. http://www.techgraffiti.com/news-airbus-a350-composites-trial-part-i.2017‐05–20.
4. Morey B. · Manufact. Eng. · 2008 · 140 · 12
5. 10.1016/j.compositesb.2011.12.00310.1016/j.compositesb.2011.12.003 ↗
6. 10.1177/002199831350206610.1177/0021998313502066 ↗
7. 10.2514/3.1161310.2514/3.11613 ↗
8. OlmedoR GürdalZ.Buckling response of laminates with spatially varying fiber orientations. In: Collection of Technical Papers‐AIAA/ASME Structures Structural Dynamics and Materials Conference Vol.22 2261–2269(1993).10.2514/6.1993-1567 ↗
9. Z.Gürdal andB.Tatting. Tow‐Placement Technology and Fabrication Issues for Laminated Composite Structures. 46th AIAA/ASME/AHS/ASC Structures Structural Dynamics & Materials Conference 2005 Austin Texas.10.2514/6.2005-2017 ↗
10. 10.2514/1.3267610.2514/1.32676 ↗
11. 10.1016/j.tws.2012.07.00810.1016/j.tws.2012.07.008 ↗
12. 10.1016/S0266-3538(02)00312-310.1016/S0266-3538(02)00312-3 ↗
13. 10.1108/0144515001035324210.1108/01445150010353242 ↗
14. 10.1016/j.compositesa.2012.02.02410.1016/j.compositesa.2012.02.024 ↗
15. Wen L.W. · Acta Aeronaut. Astronaut. Sin. · 2012 · 33 · 1
16. Duan Y.G. · Acta Aeronaut. Astronaut. Sin. · 2014 · 35 · 1
17. 10.1016/j.compstruc.2013.04.01510.1016/j.compstruc.2013.04.015 ↗
18. 10.1016/j.compstruct.2016.06.04310.1016/j.compstruct.2016.06.043 ↗
19. 10.1016/j.rcim.2017.02.00510.1016/j.rcim.2017.02.005 ↗
20. 10.1016/j.compstruct.2015.12.02510.1016/j.compstruct.2015.12.025 ↗
21. 10.1016/j.compstruct.2016.10.08110.1016/j.compstruct.2016.10.081 ↗
22. 10.2514/1.J05515910.2514/1.J055159 ↗
23. 10.1016/j.tws.2016.10.01210.1016/j.tws.2016.10.012 ↗
24. Fu H.Y. · Acta Mater. Compos. Sin. · 2017 · 8 · 1729
25. K.Wu Z.Gürdal J.Starnes. Structural Response of Compression‐Loaded Tow‐Placed Variable Stiffness Panels. In: Proceedings of the 43rd AIAA/ASME/AHS/ASC Structures Structural Dynamics and Materials Conference AIAA Denver USA 2002.10.2514/6.2002-1512 ↗
26. K.Wu andZ.Gurdal. Thermal Testing of Tow‐Placed Variable Stiffness Panels. In: Proceedings of the 42nd AIAA/ASME/AHS/ASC Structures Structural Dynamics and Materials Conference AIAA Seattle USA.2001.10.2514/6.2001-1190 ↗
27. 10.1177/002199830809767510.1177/0021998308097675 ↗
28. 10.1016/j.compstruct.2012.10.03110.1016/j.compstruct.2012.10.031 ↗
29. C.Waldhart. Analysis of Tow‐placed Variable‐stiffness Laminates. Master thesis Virginia polytechnic Institute and State University June 1996.10.2514/6.1996-1569 ↗