Results of a flight investigation to determine the zero-lift drag characteristics of a 60 degree delta wing with NACA 65-006 airfoil section and various double-wedge sections at Mach numbers from 0.7 to 1.6

Author:	Welsh, Clement J
Year:	1956
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3650
Link:	https://digital.library.unt.edu/ark:/67531/metadc55945/