The dynamic-response characteristics of a 35 degree swept-wing airplane as determined from flight measurements

Author:	Triplett, William C.
Additional Authors:	Brown, Stuart C.
Year:	1952
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-1250
Link:	https://digital.library.unt.edu/ark:/67531/metadc60636/