Multidisciplinary Performance Analysis Optimization of Subsonic Flow on Turbine in a Diffuser Duct with New experimental Göttingen 535 Airfoil Strut and Present Usual NACA 4421Airfoil Strut

Sk Sariful Islam; Badugula.Kasi Sambasiva Rao; Prof. Dr Naresh Chowdary; Prof. Dr Nagesh Naga

Volume : V, Issue : III, March - 2016

Multidisciplinary Performance Analysis Optimization of Subsonic Flow on Turbine in a Diffuser Duct with New experimental Göttingen 535 Airfoil Strut and Present Usual NACA 4421Airfoil Strut

Sk Sariful Islam, Badugula. Kasi Sambasiva Rao, Prof. Dr Naresh Chowdary, Prof. Dr Nagesh Naga

Abstract :

<p>&nbsp;A comprehensive analysis investigation on the subsonic compressible flow performance to in diffuser duct with the help of usual(NACA 4421) airfoil strut data as compared to new experimental design and analysis performance data with help of g&ouml;ttingen 535 airfoil strut on gas turbine afterburner diffuser. We try to obtain the optimum system performance during combustion processes with the help this experiment&rsquo;s. The engine performance parameters such as total pressure loss, flow properties such Mach number, flow velocity, statics pressure, swirl are compared for both the cases. In this paper we concentration on With the help of new design and flow analysis on g&ouml;ttingen 535 airfoil strut with diffuser duct can provided better performance and pressure loss improvement as compared to current using NACA 4421 airfoil strut present experimental data on afterburner diffuser duct at combustion chamber</p>