Design and performance analysis of a two-stage transonic low-reaction counter-rotating aspirated fan/compressor with inlet counter-swirl
Author:
Funder
National Natural Science Foundation of China
China Postdoctoral Science Foundation
National Science and Technology Major Project
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference39 articles.
1. The design of highly loaded axial compressors;Dickens;J. Turbomach.,2011
2. Criteria for designing low-loss and wide operation range variable inlet guide vanes;Shi;Aerosp. Sci. Technol.,2018
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