Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory

Author:	Sinnette, John T.
Additional Authors:	King, J. Austin., Schey, Oscar W.
Year:	1944
Document Type:	MAIN
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:11/E1
Series:	Wartime Report / National Advisory Committee for Aeronautics ;
Report Number:	no. E1
Subjects:	Charts, diagrams, etc
	Mathematics
	Compressors--Performance
	Axial flow compressors
	Aerofoils--Research
Link:	https://hdl.handle.net/2027/mdp.39015095014299