The subsonic static aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3. I : effects of horizontal-tail location and size on the longitudinal characteristics

Author:	Tinling, Bruce E.
Year:	1957
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-4041
Link:	https://digital.library.unt.edu/ark:/67531/metadc56477/