Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections III : comparison of blade-element performance with three levels of solidity

Author:	Schwenk, Francis C
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E55F01
Link:	https://digital.library.unt.edu/ark:/67531/metadc61336/