Evaluation of porosity effects on the mechanical properties of carbon fiber-reinforced plastic unidirectional laminates by X-ray computed tomography and mechanical testing
Source abstract
Abstract
The effects of porosity on the matrix-dominated mechanical properties of unidirectional carbon fiber-reinforced plastic composites were evaluated using X-ray computed tomography and mechanical testing. Carbon fiber-reinforced plastic plates of four porosity levels were manufactured by implementing different curing cycles. Porosity was detected by X-ray computed tomography tests, conducted on samples taken from the plates, and quantified by analyzing the computed tomography scans using the VGStudio Max software. Four different types of mechanical tests were conducted; namely, transverse tension, V-notched rail shear, three-point bending, and short-beam shear tests. The porosity analysis showed that with increasing the porosity volume fraction, the number of pores decreases, their volume increases while their shape changes from spherical or ellipsoidal to a needle-shape. The results from mechanical tests reveal that the presence of pores reduces all matrix-dominated material properties of the UniDirectional (UD) carbon fiber-reinforced plastic material. The reduction in strength is greater than the reduction in the elastic properties. Moreover, the reduction in the in-plane shear and interlaminar properties is greater than the tensile properties of the UD carbon fiber-reinforced plastic material. Between porosity contents of similar volume fraction, the one with the few large pores proved more severe than the one with the many small pores. The large standard deviation observed for some of the tests is attributed to the non-uniform dispersion of pores.
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Research context
OpenAlex topics: Mechanical Behavior of Composites · Optical measurement and interference techniques · Epoxy Resin Curing Processes
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Department of Mechanical Engineering and Aeronautics, Laboratory of Technology and Strength of Materials, University of Patras, Patras, Greece
LA composite, Beranovych, Prague 9, Czech Republic
Institute of Experimental and Applied Physics, Czech Technical University in Prague, Horska, Prague, Czech Republic
References (35)
Show source-provided references
1. 10.1016/j.compstruct.2005.02.00110.1016/j.compstruct.2005.02.001 ↗
2. 10.1016/j.compscitech.2010.09.00910.1016/j.compscitech.2010.09.009 ↗
3. 10.1016/0010-4361(92)90186-X10.1016/0010-4361(92)90186-X ↗
4. 10.1016/0010-4361(92)90187-Y10.1016/0010-4361(92)90187-Y ↗
5. Michal Tkac. Porosity development in composite carbon materials during heat treatment . PhD thesis, Norwegian University of Science and Technology, Norway, 2007. [ISSN 1503–8181].
6. 10.1016/j.compscitech.2013.06.00510.1016/j.compscitech.2013.06.005 ↗
7. 10.1177/002199831349410110.1177/0021998313494101 ↗
8. 10.1177/00219983980320160210.1177/002199839803201602 ↗
9. 10.1177/002199831454199310.1177/0021998314541993 ↗
10. 10.1016/0010-4361(95)96808-J10.1016/0010-4361(95)96808-J ↗
11. 10.1590/S1516-1439200600010001610.1590/S1516-14392006000100016 ↗
12. 10.1016/S1005-0302(11)60028-510.1016/S1005-0302(11)60028-5 ↗
13. 10.1016/0266-3538(95)00128-X10.1016/0266-3538(95)00128-X ↗
14. 10.1016/S0266-3538(01)00157-910.1016/S0266-3538(01)00157-9 ↗
15. Bowles KJ and Frimpong S. Relationship between voids and interlaminar shear strength. In: 36th SAMPE Symposium and Exhibition, San Diego, California, 15–18 April 1991, NASA technical memorandum 103643, pp. 1–20. Cleveland, OH, United States: NASA Lewis Research Center.
16. 10.1016/0263-8223(94)90044-210.1016/0263-8223(94)90044-2 ↗
17. Smith RA. Composite defects and their detection. Mater Sci Eng Vol. III .
18. 10.1016/0029-1021(75)90023-710.1016/0029-1021(75)90023-7 ↗
19. Hillger W. Determination of porosity in aerospace structures by ultrasonic pulse echo technique. In: Conference proceedings of the 8th European conference on nondestructive testing , Barcelona (Spain), 17–21 October, 2002, paper no. 10. Available at: http://www.ndt.net/article/aero2010/papers/we1a2.pdf.
20. 10.1016/S1359-8368(00)00005-610.1016/S1359-8368(00)00005-6 ↗
21. 10.1016/j.ndteint.2011.11.01110.1016/j.ndteint.2011.11.011 ↗
22. 10.1016/j.compscitech.2013.09.01910.1016/j.compscitech.2013.09.019 ↗
23. 10.1016/j.compscitech.2013.11.00410.1016/j.compscitech.2013.11.004 ↗
24. 10.1016/j.msea.2007.11.05010.1016/j.msea.2007.11.050 ↗
25. Kastner J, Plank B, Salaberger D, et al. Defect and porosity determination of fibre reinforced polymers by x-ray computed tomography. In: Proceedings of the 2nd international symposium on NDT in aerospace 2010-We.1.A.2 .
26. 10.1177/002199831349491710.1177/0021998313494917 ↗
27. 10.1177/002199831350273910.1177/0021998313502739 ↗
28. 10.1016/j.nima.2007.01.15710.1016/j.nima.2007.01.157 ↗
29. Standard test method for tensile properties of polymer matrix composite materials. Designation: D3039/D3039M-95a. American society for testing of materials (ASTM).
30. Standard test method for shear properties of composite materials by v-notched rail shear method. Designation: D7078/D7078-12. American society for testing of materials (ASTM).
31. ISO 14125:1998. Fibre-reinforced plastic composites, determination of flexural properties, English version of DIN EN ISO 14125.
32. Standard test method for short-beam strength of polymer matrix composite materials and their laminates. Designation: D2344/ D2344M-00, American society for testing of materials (ASTM).
33. VGStudio MAX Reference Manual v2.2. Volume graphics GmbH , 1998–2014 .
34. Xu L · 2009
35. Ferrari S. Image segmentation . Universita degli Studi di Milano, Elaborazione di Imagini (image processing I), academic year 2011–2012.