The effect of blade-section thickness ratio on the aerodynamic characteristics of related full-scale propellers at Mach numbers up to 0.65

Author:	Maynard, Julian D.
Year:	1949
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-1126
Link:	https://digital.library.unt.edu/ark:/67531/metadc60493/