Wind-tunnel investigation of effect of yaw on lateral-stability characteristics 3: symmetrically tapered wing at various positions on circular fuselage with and without a vertical tail

Author:	Recant, Isidore G.
Year:	1941
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-825
Link:	https://digital.library.unt.edu/ark:/67531/metadc54573/