Experimental downwash and wake characteristics at subsonic and supersonic Mach numbers behind an unswept, tapered wing, of aspect ratio 2.67 with leading-and trailing-edge flaps

Author:	Stivers, Louis S , Jr
Additional Authors:	Walker, Harold J
Year:	1951
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A51B16
Link:	https://digital.library.unt.edu/ark:/67531/metadc58738/