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By Tomoko Sano, T. S. Srivatsan

The papers during this quantity disguise a wide spectrum of issues that characterize the actually diversified nature of the sphere of composite fabrics. lately, composite fabrics have grown in energy, stature, and importance to develop into a key fabric of more advantageous clinical curiosity and resultant study into figuring out their habit for choice and secure use in a large spectrum of technology-related functions. This assortment provides learn and findings suitable to the most recent advances in composites fabrics, in particular their use in aerospace, maritime, or even land purposes. The editors have made each attempt to collect authors who placed forth contemporary advances of their examine whereas simultaneously either elaborating on and thereby bettering our winning realizing of the salient features on the topic of the technological know-how, engineering, and far-reaching technological purposes of composite materials.

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Hehr, M. Dapino, Optimized Welding Parameters of Al 6061 Ultrasonic Additive Manufactured Structures, JMR 29 (18). [11] Vishay, Measurement of Thermal Expansion Coefficient Using Strain Gages, Tech. , Micro-Measurements, tN-513-1 (2010). 11 Documentation, Dassault Systèmes Simulia Corporation, 2011. [13] P. Thamburaja, L. Anand, Polycrystalline shape-memory materials: effect of crystallographic texture, Journal of the Mechanics and Physics of Solids 49 (4) (2001) 709-737. [14] K. Kim, S. Daly, The effect of texture on stress-induced martensite formation in nickel-titanium, Smart Materials and Structures 22 (7) (2013) 075012.

No transformation happens in the region between these, and the volume fraction of phases here totally depends on previous path. The lst-cycle t r a j e c t o r y shown here is based on the present finite element simulations. The partial A-M transformation is found to be the mechanism behind the compressive strain at the end of the 1st cycle shown in Figure 10(a). It arises from the difference in 25 A-M mechanical driving forces during the reorientation stage (blue regime in Figure 6) and t h a t during in situ cooling in the composite.

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. 29 2015 Introduction The growing demands on sophisticated lightweight designs in transportation promote the market of customized materials, such as composites as well as compound materials. For the latter one attractive material combination constitutes aluminum and titanium.

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