Wind-Tunnel Flutter Tests at Mach Numbers Up to 3.0 of Boeing Wing Models for Weapons System 110A: Coord. No. AF-AM-108

Author:	Levey, G. M.
Additional Authors:	Tuovila, W. J.
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-SL57J11a
Link:	https://digital.library.unt.edu/ark:/67531/metadc64963/