Use of Blended Blade and End Wall method in compressor cascades: Definition and mechanism comparisons
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference21 articles.
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3. The use of sweep and dihedral in multistage axial flow compressor blading, part I: university research and methods development;Gallimore;J. Turbomach.,2002
4. The use of sweep and dihedral in multistage axial flow compressor blading, part II: low and high speed designs and test verification;Gallimore;J. Turbomach.,2002
5. Competing 3D mechanisms in compressor flows;Taylor;J. Turbomach.,2017
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