Full-scale wind-tunnel tests of a 35 degree sweptback-wing airplane with high-velocity blowing over the trailing-edge flaps: longitudinal and lateral stability and control

Author:	Tolhurst, William H., Jr.
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A56E24
Link:	https://digital.library.unt.edu/ark:/67531/metadc63787/