Variable nozzle turbocharger turbine performance improvement and shock wave alternation by distributing nozzle endwall clearances
Author:
Affiliation:
1. School of Mechanical Engineering, Beijing Institute of Technology, Beijing, China
2. Michigan State University, East Lansing, MI, USA
Funder
National Natural Science Foundation of China
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/0954407018757620
Reference12 articles.
1. Experimental testing of an active control turbocharger turbine inlet equipped with a sliding sleeve nozzle
2. Numerical Analysis of Nozzle Clearance's Effect on Turbine Performance
3. Study on Flow Fields in Variable Area Nozzles for Radial Turbines
4. An experimental assessment of the effects of stator vane clearance location on an automotive turbocharger turbine
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