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By Tomoko Sano, T. S. Srivatsan

The papers during this quantity hide a wide spectrum of issues that characterize the really assorted nature of the sector of composite fabrics. in recent times, composite fabrics have grown in power, stature, and value to turn into a key fabric of more desirable medical curiosity and resultant learn into knowing their habit for choice and secure use in a large spectrum of technology-related purposes. This assortment offers study and findings suitable to the most recent advances in composites fabrics, particularly their use in aerospace, maritime, or even land purposes. The editors have made each attempt to assemble authors who positioned forth contemporary advances of their study whereas at the same time either elaborating on and thereby improving our triumphing knowing of the salient facets relating to the technological know-how, engineering, and far-reaching technological functions of composite materials.

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The second aim of the study was to investigate the development of the bonding zone during processing. 5 and titanium grade 2. The bonding zones of the co-extruded samples were analyzed by scanning electron microscopy and energy dispersive X-ray analysis. The bond strength was determined by quasi-static tensile tests. Compared to the as-extruded condition an intermetallic layer was formed during heat treatment. The layer was characterized by scanning electron microscopy and electron probe micro analysis.

This will be determined through calibration. For further details regarding the development and implementation of the SMA model, the readers are referred to Ref. [13] and [8], Table 2: Material parameters of the NiTi fiber (calibrated) and Al matrix (from [4]). 6 Equilibrium transformation t e m p e r a t u r e (Κ): θ χ = 303; Latent heat of t r a n s f . / u n i t vol. ( J / c m 3 ) : λχ = 151; h -hhtu - {j C^4 (4 (Va )1/ 35 000 00 {(* Hardening matrix h. t φ= u )« ), . 0; Number of martensite CVPs: Νγ = 24; Max.

S. Srivatsan TMS (The Minerais, Metals & Materials Society), 2015 FABRICATION AND CHARACTERIZATION OF NIOBIUM-ALUMINUM COMPOSITES: EFFECT OF SINTERING TEMPERATURE Lucio Vazquez, Juan Manuel Miranda, Elizabeth Garfias and Dulce Dyolotzin Universidad Autônoma Metropolitana-Azcapotzalco, Av. San Pablo 180 Col. Reynosa Tamaulipas Mexico D. P. 7) to define the effect that sintering temperature, 390 and 550°C, had on the consolidation of the composites, and the influence on the density of the mechanical properties: hardness, elastic strength, elastic modulus, ductility, and impact toughness.

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