Abstract-The Magneto-rheological fluid is a smart fluid which changes its mechanical characteristics with varying magnetic fields. This principle of Magneto-rheological fluid is used in the human prosthesis, automotive shock absorbers, cockpit seats of military and commercial aviation etc. The purpose of this research is to synthesize an MR fluid using silicone oil as the constituent carrier fluid with other additives and to determine the coefficient of viscosity at varying magnetic field using Poiseuille's equation which is an indirect method of viscosity determination. The relationship curve between the viscosity of the synthesized fluid and the magnetic field over the varying range is plotted using the obtained results.
There have been concerted efforts towards improving the fuel efficiency of the jet engines in the past, with an aim of reducing the incomplete combustion. The process of combustion in a jet engine takes place in the combustor. A study was conducted for enhancement of air-fuel mixing process by computational analysis of an elliptically shaped combustor for a gas turbine engine. The results of computational analysis of an elliptical shape combustor were compared with a circular shape combustor used in gas turbine engines with a identical cross sectional area. The comparison of the computationally derived parameters of the two combustors i.e. temperature, pressure, and velocity are studied and analyzed. The study intends towards the comparison of the combustion efficiencies of the circular and elliptically shaped combustors. The combustion efficency of elliptical chamber is found to be 98.72% at the same time it was observed 56.26% in case of circular type combustor.
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