The target of this paper is to build up an exact model for ideal plan through outline the structure of wing that consolidate the composite (Skins) and isotropic materials (every single other structure) and contrast this and a similar wing made by changing the materials and the orientation of composite ply in skin.The ideal plan for each wing with various materials and different ply orientation can be obtained by comparing the displacement and stress on the wing. The structural design of the wing is finished with the assistance of CATIA V5, every parts modelled independently and collected in the IGS file. By using the IGS file as geometry, the Finite element modeling is completed in ANSYS and the Static analysis was done using ANSYS. In this analysis, the boundary conditions of inertia force of 1Kg and the lift force is used to simulate the wing loading on the wings. From this study, the Optimum design of the wing was found from the comparisons of stress and displacement of each material and ply combination.
The effect of molybdenum additions on the phases, microstructures, and mechanical properties of pre-alloyed Ti6Al4V was studied through the spark plasma sintering technique. Ti6Al4V-xMo (where x = 0, 2, 4, 6 wt.% of Mo) alloys were developed, and the sintered compacts were characterized in terms of their phase composition, microstructure, and mechanical properties. The results show that the equiaxed primary alpha and Widmänstatten (alpha + beta) microstructure in pre-alloyed Ti6Al4V is transformed into a duplex and globular model with the increasing content of Mo from 0 to 6%. The changing pattern of the microstructure of the sample strongly influences the properties of the material. The solid solution hardening element such as Mo enhances mechanical properties such as yield strength, ultimate tensile strength, ductility, and hardness compared with the pre-alloyed Ti6Al4V alloy.
Spark plasma sintering provides faster heating that can create fully, or near fully, dense samples without significant grain growth. In this study, pre-alloyed Ti-6Al-4 V powder compact samples produced through field assisted sintering in a spark plasma sintering machine are compared as a function of consolidation temperature. The effect of sintering temperature on the densification mechanism, microstructural evolution and mechanical properties of spark plasma sintered Ti-6Al-4 V alloy compacts was investigated in detail. The compact, sintered at 1100 °C, exhibited near net density, highest hardness and strength as compared to the other compacts processed at a temperature lower than 1100 °C.
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