Control of compressor tip leakage flow using plasma actuation
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference30 articles.
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2. Zonal detached-eddy simulation applied to the tip-clearance flow in an axial compressor;Riéra;AIAA J.,2016
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4. Effects of rotor tip blade loading variation on compressor stage performance;Tiralap;J. Turbomach.,2017
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