Aerodynamic Characteristics of Tapered Wings Having Aspect Ratios of 4, 6, and 8, Quarter-Chord Lines Swept Back 45 Degrees, and NACA 63(Sub 1)a012 Airfoil Sections: Transonic-Bump Method

Author:	Polhamus, Edward C.
Year:	1951
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L51C26
Link:	https://digital.library.unt.edu/ark:/67531/metadc58773/