An investigation of a lifting 10-percent-thick symmetrical double-wedge airfoil at mach number up to 1

Author:	Humphreys, Milton D
Year:	1954
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3306
Link:	https://digital.library.unt.edu/ark:/67531/metadc57312/