Wing-Tunnel Investigation of Effects of Various Aerodynamic Balance Shapes and Sweepback on Control-Surface Characteristics of Semispan Tail Surfaces With NACA 0009, 0015, 66-009, 66(215)-014, and Circular-Arc Airfoil Sections

Author:	Harper, John J.
Year:	1951
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2495
Link:	https://digital.library.unt.edu/ark:/67531/metadc55844/