Experimental investigation of an axial-flow compressor inlet stage operating at transonic relative inlet Mach numbers III : blade-row performance of stage with transonic rotor and subsonic stator at corrected tip speeds of 800 and 1000 feet per secon

Author:	Schwenk, Francis C
Additional Authors:	Lieblein, Seymour
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E53G17
Link:	https://digital.library.unt.edu/ark:/67531/metadc59687/