Effect of Blade-Section Camber on Aerodynamic Characteristics of Full-Scale Supersonic-Type Propellers at Mach Numbers to 1.04

Author:	Maynard, Julian D.
Additional Authors:	Swihart, John M.
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L56E10
Link:	https://digital.library.unt.edu/ark:/67531/metadc62729/