Issue 53

P. Fathi, Frattura ed Integrità Strutturale, 53 (2020) 457-473; DOI: 10.3221/IGF-ESIS.53.36 461 Standard DIN 53448 ISO 8256 Dimensions (mm) Type 1B 10x80 Type 2 10x60 Type 4 15x80 Type 1 10x80 Type 2 10x60 Type 3 15x80 Type 4 10x60 Type 5 15x80 Velocity (m / s) 2.9 2.9 2.9 3.7 2.9 3.7 Vise Models 6545 .760 & 6845.07 5 .760 & .926 .760 & 6845.07 5 .760 .926 .760 & 6845.075 Mobile Clamp Models 6845 .080 .081 .081 .082 .082 .083 .281 .080 .081 .081 .082 .082 .083 .281 .750 .755 .765 .815 Hammer Models 6545 .020 .021 .022 .023 .023 .926 .020 .021 .022 .023 .023 .926 .020 .021 .022 .023 Starting angle weight dropper 6957.075 for 6957.000, 6958.000 & 6959.000 Potential Energy (J) 2 4 7.5 15 25 50 2 4 7.5 15 25 50 2, 4, 7.5 15 & 25 Table 3: Tensile Impact Details. E XPERIMENTAL S TUDY ne of the most important properties is the strength of the composites in mechanical coupling. For this purpose, the method of fabricating and conducting experimental tests on composite specimen with mechanical coupling (PIN) under tensile loading is investigated. First, we will explain how to build a multilayer, and then prepare it for impact traction testing. In this study, a composite and symmetrical plate (length L, width W, thickness t) with materials consisting of fiberglass fabrics in 0° and 90° directions and epoxy resin were fabricated. The plate is investigated from 8 layers with a layer of [0°,90°, - 45° and 45°] s which is symmetric and isotropic with respect to the layer. The geometry of the plate has a hole d in diameter that is located exactly at the centerline of the plate and at a distance from one edge. In this study, five complete specimens were made according to standard dimensions, and the reason is to perform at least five tests according to D1822 standard, which should test at least five fragments in each condition unless valid results can be obtained with fewer tests [15]. After preparation of the specimens, the impact tensile test is performed. Tab. 4 Mechanical properties of composite material is shown. O