Wind Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics: [Part] 4 - Symmetrically Tapered Wing With a Circular Fuselage Having a Wedge-Shaped Rear and a Vertical Tail

Author:	Recant, I. G.
Year:	1942
Document Type:	N/A
Series:	NACA Wartime Reports
Report Number:	NACA-WR-L-520, NACA-ARR
Link:	https://digital.library.unt.edu/ark:/67531/metadc61016/