Aerodynamic characteristics at subsonic and transonic speeds of a 42.7 degree sweptback wing model having an aileron with finite trailing-edge thickness

Author:	Turner, Thomas R.
Additional Authors:	Lockwood, Vernard E.
Year:	1949
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L8K02
Link:	https://digital.library.unt.edu/ark:/67531/metadc57819/