IMPROVING AND ANALYSIS TURBINE WHEEL OF TURBOCHARGER FOR HIGH-PERFORMANCE ENGINES

Author(s): 

Mohand Mosa Mohammad1, Ahmed Esmael Mohan2, Hiyam Adil Habeeb2

Affiliation(s): 

1Mussaib Technical Institute, Al-Furat Al-Awsat Technical University, Babylon, Iraq.

2Technical Collage/ Al-mussaib, Al-Furat Al-Awsat Technical University, Babylon, Iraq.

This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

A turbocharger performance of exhaust gas turbine on the diesel engines are studied the turbine driven compressor that is used for increasing air flow rate into internal combustion engine the angle of Blade effect on the flow field of turbine wheel. Angle of Blade of turbine wheel analyzed Based on the theory Computational Fluid Dynamics (CFD). How the various blade angle of turbine wheel due to optimization on flow field along the blade and leads to optimization in the pressure and velocity. Blade angle studied is conducted for understand the flow behavior in order to minimize the effects blade angle. in this paper dealing The Analyses the flow field along the blade passage of the turbine wheel for the turbocharger and study the effect flow field at different blade angle for turbine wheel outlet blade angle, β = 650, 450 and 350.