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pro vyhledávání: '"Lim Hong Ngiap"'
Publikováno v:
International Journal of Rotating Machinery, Vol 2005, Iss 2, Pp 117-127 (2005)
An improved integral method is proposed and developed for the quantitative prediction of distorted inlet flow propagation through axial compressor. The novel integral method is formulated using more appropriate and practical airfoil characteristics,
Externí odkaz:
https://doaj.org/article/9bd38049d61e49dbbdd2b72d75e7dbd1
