Abstract
This paper is devoted to the experimental study of polymeric composite specimens, with various types of reinforcement, in order to evaluate the breaking strength of specimens with open holes when undergoing uniaxial compression and tensile tests. Four types of interlaced 3D woven preforms were considered (orthogonal, orthogonal combined, with pairwise inter-layer reinforcement, and with pairwise inter-layer reinforcement and a longitudinal layer), with a layered preform used for comparison. Tensile tests of solid specimens without a hole, under ASTM D 3039, and of specimens with an open hole, under ASTM D 5766, were carried out using the Instron 5989 universal electromechanical testing system. Movements and strains on the specimen surface were recorded using a Vic-3D contactless optical video system and the digital images correlation method (DIC). For all the series of carbon fiber tension specimens, strain and stress diagrams, mechanical characteristics, and statistical processing for 10 specimens were obtained. The paper evaluated deformation fields for certain points in time; the obtained fields showed an irregular distribution of deformation and dependency on types of reinforcing fibers. A coefficient of strength variation is introduced, which is defined as a ratio of the ultimate stress limits obtained on solid samples with and without open holes. Within the framework of ASTM D 5766, when calculating the ultimate stress, the hole is not taken into account, and the paper shows that for certain structures a hole cannot be excluded. The hole size must not be neglected when calculating the ultimate stress.
Highlights
For all the series of carbon fiber tension specimens tested under ASTM D 3039, strain and stress diagrams (Figure 3), the ultimate strength, and statistical processing for 10 specimens (Table 2) were obtained
The results show that the behavior of specimens with an open hole, with reinforcement types 1, 4, and 5, remained linear-elastic until failure
This work included a series of experimental studies of strength in structural carbon fibers with various reinforcement types in tension tests with and without an open hole
Summary
Publisher’s Note: MDPI stays neutral with regard to jurisdictional claims in published maps and institutional affiliations. An obvious disadvantage of conventional polymeric composite materials, in the form of fabric-based laminates, is their relatively low inter-layer strength. Nowadays, spatialreinforced fillers or 3D fabrics are proposed to prevent this. Multi-layered carbon fabrics of various weavings are used as reinforcement materials for carbon fibers, operating under complex conditions of high-speed aerodynamic flows, vibrations, and high temperatures
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