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Tensile properties analysis composites

The main experimental methodology used is to directly characterize the tensile properties of CNTs/polymer composites by conventional pull tests (e.g. with Instron tensile testers). Similarly, dynamic mechanical analysis (DMA) and thermal mechanical analysis (TMA) were also applied to investigate the tensile strength and tensile modulus. With these tensile tests, the ultimate tensile strength, tensile modulus and elongation to break of composites can be determined from the tensile strain-stress curve. [Pg.395]

Several authors have analyzed the miscibility of iPP and PB-1, by means of different analytical approaches. Piloz et al. (16) found a single, composition-dependent, glass transition behavior for these blends, and concluded that they are compatible in the amorphous state. Sjegmann (17,18) reported that the composition dependence of tensile properties evidences a high degree of compatibility of iPP and PB-1 and observed a marked effect of the composition on the morphology of melt-crystallized samples. Conversely, the analysis of the crystallized blends indicates the presence of separated crystal phases of the two polymers, even if a mutual influence during the crystallization cannot be excluded. [Pg.122]

Ultimate tensile strength, stifihess, and strain-to-failure were determined quasi-statically for each class of as-received material in accordance with ASTM D 3039 Standard Test Method for Tensile Properties of Polymer Matrix Composite Materials using a deflection rate of 2.5 mm/min (0.10 in./min). A total of thirty samples were tested, ten of each material type. In addition, two samples of each material were set aside for crack density analysis using x-ray and optical microscopy techniques. [Pg.496]

For many fiber-polymer systems (L/D) is in the range 10 50. From this analysis, it is evident that fiber length is important to the development of maximum tensile properties in the composite. It is also apparent that changes in the composite tensile strength are monotonically dependent on fiber concentration. [Pg.811]

Fig. 7 illustrates Chapman s treatment of the mechanics of this composite system. The system is treated as a set of zones consisting of fibril and matrix elements. Originally, this was introduced as a way of simplifying the analysis, but, the later identification of the links through IF protein tails makes it a more realistic model than continuous coupling of fibrils and matrix. Up to 2% extension, most of the tension is taken by the fibrils, but, when the critical stress is reached, the IF in one zone, which will be selected due to statistical variability or random thermal vibration, opens from a to P form. Stress, which reduces to the equilibrium value in the IF, is transferred to the associated matrix. Between 2% and 30% extension, zones continue to open. Above 30%, all zones have opened and further extension increases the stress on the matrix. In recovery, there is no critical phenomenon, so that all zones contract uniformly until the initial extension curve is joined. The predicted stress-strain curve is shown by the thick line marked with aiTows in Fig. 6b. With an appropriate. set of input parameters, for most of which there is independent support, the predicted response agrees well with the experimental curves in Fig. 6a. The main difference is that there is a finite slope in the yield region, but this is explained by variability along the fibre. The C/H model can be extended to cover other aspects of the tensile properties of wool, such as the influence of humidity, time dependence and setting. Fig. 7 illustrates Chapman s treatment of the mechanics of this composite system. The system is treated as a set of zones consisting of fibril and matrix elements. Originally, this was introduced as a way of simplifying the analysis, but, the later identification of the links through IF protein tails makes it a more realistic model than continuous coupling of fibrils and matrix. Up to 2% extension, most of the tension is taken by the fibrils, but, when the critical stress is reached, the IF in one zone, which will be selected due to statistical variability or random thermal vibration, opens from a to P form. Stress, which reduces to the equilibrium value in the IF, is transferred to the associated matrix. Between 2% and 30% extension, zones continue to open. Above 30%, all zones have opened and further extension increases the stress on the matrix. In recovery, there is no critical phenomenon, so that all zones contract uniformly until the initial extension curve is joined. The predicted stress-strain curve is shown by the thick line marked with aiTows in Fig. 6b. With an appropriate. set of input parameters, for most of which there is independent support, the predicted response agrees well with the experimental curves in Fig. 6a. The main difference is that there is a finite slope in the yield region, but this is explained by variability along the fibre. The C/H model can be extended to cover other aspects of the tensile properties of wool, such as the influence of humidity, time dependence and setting.
Zhou et al. [173] studied the effects of surface treatment of calcium carbonate particles with sulfonated polyether ether ketone on the mechanical and thermal properties of composites with polyether ether ketone in various proportions prepared using a twin-screw extruder. These workers used tensile, impact, and flexural testing, thermogravimetric analysis, differential scanning calorimetry, and scanning electron microscopy. The influences of filler particle, loading, and surface treatment on deformation and crystallinity of polyether ether ketone were discussed. [Pg.82]

The FTIR and XPS analysis showed that site-interaction between NH and OH groups of PPy and BC components, respectively, was operative in both the composites. The affinity between functional groups of PPy-FeClj and BC was higher than that found for BC/PPy-APS composite. In addition, the tensile properties (tensile strength 40 MPa) were also influenced by the chemical affinity of both the components in the composites [62]. [Pg.144]

Permeability Porosity Pore size Thickness Chemical composition Thermal stability Mechanical strength Electrical resistivity, voltage drop, air flow Calculated from dimensions, basis weight, and skeletal density Image analysis, Hg porometry Micrometer Atomic absorption, differential scanning calorimetry, others Hot electrical resistivity, thermal-mechanical analysis Tensile properties, puncture strength... [Pg.709]

The Applicable Documents section lists all the relevant documents that form part of this specification. Two SAE publications are listed in AMS 5663, which has a composition similar to that of commercial 718 nickel alloy— AMS 2261, "Tolerances, Nickel, Nickel Alloy, and Cobalt Alloy Bars, Rods, and Wire," and AMS 2269, "Chemical Check Analysis Limits, Nickel, Nickel Alloys, and Cobalt Alloys"—along with seven other AMS publications. Also, two ASTM publications, ASTM E8M, "Tension Testing of Metallic Materials (Metric)," and ASTM ElO, "Brinell Hardness of Metallic Materials," are listed, along with seven other ASTM publications. Therefore, to claim the conformance of AMS 5663 to the OEM design data, the comparative tensile properties should be evaluated in accordance with ASTM E8M (or its equivalence), which is part of the design document. [Pg.146]


See other pages where Tensile properties analysis composites is mentioned: [Pg.31]    [Pg.367]    [Pg.373]    [Pg.263]    [Pg.588]    [Pg.176]    [Pg.588]    [Pg.56]    [Pg.331]    [Pg.171]    [Pg.349]    [Pg.600]    [Pg.183]    [Pg.188]    [Pg.272]    [Pg.226]    [Pg.291]    [Pg.22]    [Pg.358]    [Pg.371]    [Pg.378]    [Pg.250]    [Pg.259]    [Pg.22]    [Pg.225]    [Pg.387]    [Pg.267]    [Pg.36]    [Pg.9]    [Pg.264]    [Pg.141]    [Pg.201]    [Pg.350]    [Pg.366]    [Pg.496]    [Pg.62]    [Pg.74]    [Pg.1649]   


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