The effect of thickness ratio on section thrust distribution as determined from a study of wake surveys of the NACA 4-(0)(03)-045 and 4-(0)(08)-045 two-blade propellers up to forward Mach numbers of 0.925

Author:	Harrison, Daniel E
Year:	1951
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L51B05
Link:	https://digital.library.unt.edu/ark:/67531/metadc58934/