High-speed tests of an airfoil section cambered to have critical Mach numbers higher than those attainable with a uniform-load mean line

Author:	Graham, Donald J
Year:	1947
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-1396
Link:	https://digital.library.unt.edu/ark:/67531/metadc55477/