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pro vyhledávání: '"Prithesh Pinto"'
Autor:
Prithesh Pinto, Srinivas G
Publikováno v:
Cogent Engineering, Vol 11, Iss 1 (2024)
This research article focuses on improving the efficiency of an axial flow compressor stage, enhancing the stall margin, and optimizing flow parameters. Utilizing the NACA 65 series rotor airfoil with 12 blades, the study employs numerical simulation
Externí odkaz:
https://doaj.org/article/339cde4baf934698b172bde447b2181b
