Wind-Tunnel Investigation at High Subsonic Speeds of a Spoiler-Slot Deflector Combination on an NACA 65A006 Wing With Quarter-Chord Line Swept Back 32.6 Degrees

Author:	Vogler, Raymond D.
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L53D17
Link:	https://digital.library.unt.edu/ark:/67531/metadc59599/