Wind-Tunnel and Flight Investigations of the Use of Leading-Edge Area Suction for the Purpose of Increasing the Maximum Lift Coefficient of a 35 Degree Swept-Wing Airplane

Author:	Holzhauser, Curt A.
Year:	1956
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-1276
Link:	https://digital.library.unt.edu/ark:/67531/metadc60669/