The Subsonic Lateral and Longitudinal Static Stability Characteristics Up to Large Angles of Sideslip for a Triangular-Wing Airplane Model Having a Ventral Fin

Author:	Buell, Donald A.
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A56H06
Link:	https://digital.library.unt.edu/ark:/67531/metadc53199/