Experimental and predicted longitudinal and lateral-directional response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet

Author:	Cole, Henry A., Jr.
Additional Authors:	Brown, Stuart C.
Year:	1957
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-1330
Link:	https://digital.library.unt.edu/ark:/67531/metadc60731/