In this paper, two kinds of roving glass woven fabrics of different FAW (Fabric Area Weight), 570 g/m² and 800 g/m², were adopted. Unsaturated polyester resin (150 HRBQTNA, Showa Denko K.K.) was adopted as the matrix. The glass roving clothes manufactured by Hokuriku Fiberglass Co., Ltd are in plain structure as showing in Figure 1. The one with lighter FAW is named as Type A (570 g/m²), and the heavier one is named as Type B (800 g/m²). Detailed information of the glass fiber bundle (Nitto Boseki Co., Ltd.), such as linear density and yarn density, is listed in Table 1. It can be seen that fiber bundles of same linear density were used while the ends per inch for the warp direction and the picks per inch in the weft direction are different. And Type A is of relatively higher yarn density. In this study, the warp direction is defined as 0 degree and the weft direction as 90 degree.

The glass roving cloth reinforced composites were manufactured by hand lay-up molding method for only 1 ply for the purpose of reveal the crack

propagation and fracture mechanism. After the fabrication, the composite board was cut to the size of 200 mm × 20 mm (length × width) according to ASTM D3039 according to 6 orientations 0˚/5˚/10˚/80˚/85˚/90˚. The thickness of Type A is approximately 0.60 mm, while Type B is approximately 0.65 mm, a little thicker than Type A. Cross-sectional observation was carried out and the crimp percentage for both the 0 and 90 degree directions of Type A and Type B was calculated, and is showed in Table 1. Crimps are formed because of the weaving process. It can be seen from Figure 1 and Table 1 that Type A is of relatively higher yarn density, and the crimp ratio of Type A is slightly higher than that of Type B. It means for the same unit length, the fiber bundle length of Type A is longer than that of Type B.

Mechanical investigation of the tensile properties was carried out on specimens in 6 degrees 0˚/5˚/10˚/80˚/85˚/90˚. The tensile tests were carried out on an Instron universal testing machine at a speed of 1 mm/min and the test room temperature was 22˚C according to the ASTM D3039. (Specimen number N = 3). For 0˚ and 90˚, which are also defined as on-axis cases, the fracture progress during the tensile test has been observed by take video. During the tensile tests, an AE (acoustic emission) device was used in order to detect when the initial fracture occurred. A video was also shot in order to understand the fracture process. In the photographs collected from the video at different strain stages, three main periods can be identified to depict the fracture process. Combined with the AE data and the video footage, the initial fracture behavior has been discussed. For 5˚/10˚/80˚/85˚, which are defined as off-axis cases, tensile modulus, tensile strength were also tested and discussed. Besides, the difference of deferent degrees, and the comparison between Type A and B has been discussed and summarized.

The stress-stain curves are illustrated in Figure 2, and details of the results of the tensile tests are shown in Figure 3, and Table 2. It can be known that the tensile modulus of Type B is similar with Type A, and the tensile modulus of the 90 degree direction is higher than that of the 0 degree direction.

On the other hand, the tensile strength of Type B turned out to be much higher than that of Type A for both the 0 and 90 degree directions. The fiber bundle cross section area ratio of Type A and Type B was calculated and this value could be referred as an index similarly with V_f (volume fraction of reinforcing fibers). The result showed the value of Type A is slightly higher than that of Type B, which is revealing that Type A might get higher tensile strength. However, it does not agree with the tensile strength result.

When it comes to the elongation, it can be known from Table 2 that the

elongation rate for Type B is higher than Type A. This would be taken as one of the reasons for the high tensile strength of Type B. But the reason why Type B achieved higher elongation should be found out firstly because the crimp ratio of Type B is lower than that of Type A which indicated Type A should have got higher elongation.

Otherwise, the initial fracture results detected by acoustic emission showing in Table 2 revealed that for both Type A and Type B in both 0 degree and 90 degree directions, the initial fracture stress values are similar.

In order to decide where exactly the initial fracture happened, specimens were under tensile testing and stretched to 1.3 times the initial fracture stress and stopped. Then observation was carried out on the longitudinal cross section by optical microscopy. From the photographs shown in Figure 4, it can be clearly seen that transverse cracks first occurred in the transverse fiber bundles, which can be regarded as contacted to the initial fracture stress.

The fracture processes are illustrated by still images from the video in Figure 5. It can be obviously observed that transverse cracks appeared within the transverse fiber bundles at the very early stage. And with the transverse crack increased, another type of cracks in wave shape began to appear between transverse fiber bundles. The schemas of the transverse crack and the wave shape crack are illustrated in Figure 6(a) and Figure 6(b). The wave shape cracks formed because of the existence of the crimp. With the loading going higher, the fiber bundles along the load direction were stretched and had a tendency to become straight, which gave a compressive stress to the transverse fiber bundles. The resin rich area between the transverse fiber bundles was compressed and wave shape cracks formed along the iso-stress surface, which could be the direct reason leading to the final fiber bundle breaking. The wave shape cracks showing in Figure 6(b) are characteristic cracks appearing in woven fabric reinforced composited because of the woven structure.

There were several period before the final fracture can be summarized during the fracture period for both Type A and Type B involved with transverse cracks and wave shape cracks. Schemas are summarized and illustrated in Figure 7(a) for Type A and Figure 7(b) for Type B.

1) Firstly, for both Type A and Type B, transverse cracks occurred firstly in the transverse fiber bundles, and then the number of transverse cracks increases. During this period, the interface between the glass fibers and the resin is subjected to most of the load. White line of cracks can be observed in the cross section area of the warp and weft fiber bundles.

2) During this period, the interface between the glass fibers and the resin is still the main carrier of most of the load. White cracks increased gradually until the cracks went through the transverse fiber bundles. It can be seen that transverse cracks within Type B are much finer than those in Type A.

3) Because of the tendency of the fiber bundle in the crimp to be stretched, the cross section of the warp fiber bundle and weft fiber bundle is compressed and wave shape cracks began to show up both for Type A and Type B. During this period, the interface between the glass fiber and the resin still carried the most of the load but the longitudinal fiber bundles are beginning to take most of the load. More cracks in wave shapes appeared between the transvers fiber bundles were observed in Type A and then increased from Figure 7(a). While for Type B, very few wave shape cracks were also observed, and more fine transverse cracks increased.

4) Fourthly, the longitudinal fiber bundles become carrying the most of the load and finally leading to the fracture of the specimen. It was obviously observed that much more wave shape cracks in Type A and propagated in transverse directions. However for Type B, wave shape cracks did not increase much, and plenty of fine transverse cracks were observed within the transverse fiber bundles.

When comparing Type A with Type B, the difference was observed from the second period. In the case of Type B, more and finer cracks were observed, while for Type A, more wave shape cracks propagated during the third and fourth period. AE results showed in Figure 8. It can been seen that the accumulated AE conus of Type A increased faster than that of Type B and kept higher above Type B. Comparing observation results with AE results, it can be considered that the wave shape cracks resulted in the main fracture and finally leading to the fiber bundle breaking along the load direction. Even the crimp ratio of Type A is

higher than that of Type B, the wave shape cracks led to fiber bundle breaking and specimen of Type A came to final fracture before it achieved a high elongation. On the contrast, the higher fiber bundle tex and lower crimp ratio of Type B makes it more tolerant with transverse cracks, and it is considered the specimen was stretched smoothly finally with a higher elongation than Type A.

Higher crimp ratio might lead a tendency to fierce wave shape cracks and result in a low tensile strength. But it is also predictable that the fabric reinforcement with a very low crimp ratio will also not achieve good tensile properties because of the low fiber volume fraction. It is considered that for woven fabric reinforced composites, there is a critical crimp ratio which contributes to better tensile properties.

Tensile test was also carried out on specimens of 5˚/10˚/80˚/85˚and the tensile results were summarized in Table 3.

The summary of tensile modulus and strength of all 6 degrees of 0˚/5˚/10˚/80˚/85˚/90˚ are illustrated in Figure 9 and Figure 10 separately. Comparing to Figure 7 and Figure 8, difference between on-axis and off axis can be seen obviously, that specimens of off-axis have much lower tensile modulus and strength. Even in the case of 5 degree and 85 degree, tensile modulus and tensile strength decreased dramatically comparing with 0 degree and 90 degree, which can be considered as a result of the shear stress.

The photographs of fractured specimens of Type A and Type B after the tensile test were shown in Figure 11 and Figure 12 separately. It can be seen from the photograph that the fracture of 5 degree and 85 degree seemed to be fiercer than that of 10 degree and 80 degree. The fracture schema is illustrated in Figure 13. For 5 degree and 85 degree, cracks propagated along fiber bundles and ultimate fiber fracture happened with the fiber bundle split up. It seems no big difference between Type A and Type B. While it also can be observed from the schema

that, in the case of 10 degree and 80 degree, especially for Type B, it can be observed that less fiber was pulled out and split, which revealed that the fiber bundle in the loading direction did not take most of the loading. And the shear stress played an important role during the tensile test, leading to the ultimate fracture of the specimen, which can be considered as the reason of the low strength in the case of the 10degree and 80 degree. Especially for Type B, there are very few fiber bundles pulled out and split in the case of the 10degree and 80 degree, and contacted with the tensile strength result which showing a decrease of more than 45% comparing with 5 degree and 85 degree.