Wing-tunnel investigation at high subsonic speeds of the lateral-control characteristics of an aileron and a stepped spoiler on a wing with leading edge swept back 51.3 degrees

Author:	Schneiter, Leslie E
Year:	1949
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L9D06
Link:	https://digital.library.unt.edu/ark:/67531/metadc58204/