Theoretical effect of inlet hub-tip-radius ratio and design specific mass flow on design performance of axial-flow compressors

Author:	Wu, Chung-Hua
Additional Authors:	Sinnette, John T
Year:	1950
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2068
Link:	https://digital.library.unt.edu/ark:/67531/metadc55431/