Investigation of Effect of Sideslip on Lateral Stability Characteristics 2: Rectangular Midwing on Circular Fuselage With Variations in Vertical-Tail Area and Fuselage Length With and Without Horizontal Tail Surface

Author:	Hollingworth, Thomas A.
Year:	1945
Document Type:	N/A
Series:	NACA Wartime Reports
Report Number:	NACA-WR-L-8, NACA-ARR-L5C13
Link:	https://digital.library.unt.edu/ark:/67531/metadc60981/