OPTIMIZE AND ANALYSIS COMPRESSOR WHEEL OF TURBO CHARGER

Author(s): 
Ali Salh Sawadi1, Mohammed Mohsin Shkhair2, Riyad Jassim Tilefih1

Affiliation(s): 
1Al-Furat Al-Awsat Technical University, Najaf Technical Institute, Al-Najaf, Iraq
2Southern Technical University, Shatra Technical Institute, Nasiriyah, Iraq
*Corresponding Author Email: alialkazraji5@gmail.com

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.

Blade angle effect on flow field of the compressor wheel. Blade angle of compressor wheel will be analyses computationally by CFD. How the different blade angle of compressor wheel causes the effect on flow field along the blade passage and leads to variation of pressure and efficiency of the wheel. Blade angle studies are conducted to understand the flow behavior in order to minimize the effects of blade angle. Through this paper an attempt is being made to address the following:

1. Analyze the flow field along the blade passage of the compressor wheel of a turbocharger.
2. To study the effect of flow field for the different blade angle. For Compressor wheel inlet blade angle, β1 = 350, 450 and 650.