Experimental investigation of aerodynamically balanced trailing-edge control surfaces on an aspect ratio 2 triangular wing at subsonic and supersonic speeds

Author:	Boyd, John W.
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A52L04
Link:	https://digital.library.unt.edu/ark:/67531/metadc64994/