Numerical analysis for impacts of nozzle end-clearances on aerodynamic performance and forced response in a VNT turbine-Reference-Cited by-同舟云学术

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Numerical analysis for impacts of nozzle end-clearances on aerodynamic performance and forced response in a VNT turbine

Published:2018-05 Issue:5 Volume:31 Page:1030-1040
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

ZHAO Ben,WANG Leilei,HOU Hongjun

Funder

Natural Science Foundation of Hebei Province of China

Program of Science and Technology Research and Development of Handan of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference21 articles.

1. A review of the application of variable geometry turbines to the downsized gasoline engine;Tang;Int J Engine Res,2015

2. Variable geometry turbocharger technologies for exhaust energy recovery and boosting – a review;Feneley;Renew Sustain Energy Rev,2017

3. Numerical analysis of nozzle clearance's effect on turbine performance;Hu;Chin J Mech Eng-en,2011

4. Walkingshaw J, Spence S, Ehrhard J, Thornhill D. A numerical study of the flow fields in a highly off-design variable geometry turbine, 2010. ASME; Glasgow, Report No.: GT2010-22669.

5. Tamaki H, Goto S, Unno M, Iwakami A. The effect of clearance flow of variable area nozzles on radial turbine performance, 2008. ASME; Berlin, Report No. GT2008-50461.

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