A novel clocking effect between inlet bend and volute in an automotive turbocharging system

Author:

Zhao Ben,Yang Ce,Hu Liangjun,Li Du,Chen Shan

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Reference19 articles.

1. K. Kim et al., The inlet flow structure of a centrifugal compressor stage and its influence on the compressor performance, Journal of Fluids Engineering, 125 (3) (2003) 779–785.

2. C. Yang, B. Zhao, C. C. Ma, D. Lao and M. Zhou, Effect of the different geometrical inlet pile on the high speed centrifugal compressor, ASME Turbo Expo 2013: Power for land, Sea, and Air, San Antonio, USA, July 3-7, ASME Paper, GT2013-94254 (2013).

3. G. J. Walker and A. R. Oliver, The effect of interaction between wakes from blade rows in an axial flow compressor on the noise generated by blade interaction, ASME Paper No. 72-GT-15 (1972).

4. F. W. Huber et al., Performance improvement through indexing of turbine airfoils: Part I-Experimental investigation, ASME Journal of Turbomachinery, 118 (3) (1995) 630–635.

5. D. J. Dorney, O. P. Sharma and K. L. Gundy-burlet, Physics of airfoil clocking in a high-speed axial compressor, ASME Paper 98-GT-82.

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