Effect of leading-edge chord-extensions on subsonic and transonic aerodynamic characteristics of three models having 45 degrees sweptback wings of aspect ratio 4

Author:	Goodson, Kenneth W
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L52K21
Link:	https://digital.library.unt.edu/ark:/67531/metadc59460/