Effect of Compressibility and Camber as Determined From an Investigation of the NACA 4-(3)(08)-03 and 4-(5)(08)-03 Two-Blade Propellers Up to Forward Mach Numbers of 0.925

Author:	Carmel, Melvin M.
Additional Authors:	Morgan, Francis G., Jr.
Year:	1950
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L50D28
Link:	https://digital.library.unt.edu/ark:/67531/metadc58435/