Investigation of 10-Stage Axial-Flow X24C-2 Compressor, 1, Performance at Inlet Pressure of 21 Inches Mercury Absolute and Inlet Temperature of 538 Degrees R

Author:	Schum, Harold J.
Year:	1947
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E7G11
Link:	https://digital.library.unt.edu/ark:/67531/metadc63835/