Aerodynamic Design Optimization of a Micro Radial Compressor of a Turbocharger

This study presents an aerodynamic design optimization of a micro radial compressor impeller on a turbocharger used in a 0.8 L two-cylinder gasoline engine. In the conventional design optimization of the impeller, the hub and shroud curve of the main blade is commonly parameterized with a beta distr...

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Bibliographic Details
Main Authors: Omer Faruk Atac, Jeong-Eui Yun, Taehyun Noh
Format: Article
Language:English
Published: MDPI AG 2018-07-01
Series:Energies
Subjects:
Online Access:http://www.mdpi.com/1996-1073/11/7/1827