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Design method for turbomachine blades with finite thickness by the circulation method
J. Jiang,
T. Dang
Department of Mechanical & Aerospace Engineering
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Article
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peer-review
9
Scopus citations
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Engineering & Materials Science
Turbomachine blades
100%
Cambers
65%
Incompressible flow
63%
Compressors
45%
Turbines
40%