Tests of a 0.30-scale semispan model of the Douglas XTB2D-1 airplane wing and fuselage combination in the NACA 19-foot pressure tunnel 2: roll-flap positioning and lateral-control investigation

Author:	Spooner, Stanley H.
Additional Authors:	Ashworth, C. Dixon
Year:	1944
Document Type:	N/A
Series:	NACA Wartime Reports
Report Number:	NACA-WR-L-564, NACA-MR
Link:	https://digital.library.unt.edu/ark:/67531/metadc61208/