Two stall stages in a centrifugal compressor with a vaneless diffuser
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference46 articles.
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2. Flow instability suppression and deep surge delay by non-axisymmetric vaned diffuser in a centrifugal compressor;Sun;Aerosp. Sci. Technol.,2019
3. Compressor surge based on a 1D-3D coupled method – part 2: surge investigation;Huang;Aerosp. Sci. Technol.,2019
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