Aerodynamic Load Distribution on a 45 Degree Sweptback Wing With Leading-Edge Chord-Extensions at Transonic Speeds, Including Effects of a Spoiler-Slot-Deflector Aileron

Author:	Schmeer, James W.
Additional Authors:	Whitcomb, Charles F.
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L57L02
Link:	https://digital.library.unt.edu/ark:/67531/metadc63905/