Wind-Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics 5: Symmetrically Tapered Wing With a Circular Fuselage Having a Horizontal and a Vertical Tail

Author:	Wallace, Arthur R.
Year:	1943
Document Type:	N/A
Series:	NACA Wartime Reports
Report Number:	NACA-WR-L-459, NACA-ARR-3F23
Link:	https://digital.library.unt.edu/ark:/67531/metadc61017/