Investigation of Reynolds number effects on flow stability of a transonic compressor using a dynamic mode decomposition method
Author:
Funder
National Major Science and Technology Projects of China
National Natural Science Foundation of China
Publisher
Elsevier BV
Reference47 articles.
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2. The influence of Reynolds number and roughness on the efficiency of axial and centrifugal fans—a physically based scaling method;Pelz;ASME J. Eng. Gas Turbines Power,2013
3. Experimental and analytical investigation of the effects of Reynolds number and blade surface roughness on multistage axial flow compressors;Schaffler;J. Eng. Gas Turbines Power,1980
4. Stalling pressure rise capability of axial flow compressor stages;Koch;J. Eng. Power,1981
5. An improved stall prediction model for axial compressor stage based on diffuser analogy;Li;Aerosp. Sci. Technol,2022
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