Static longitudinal and lateral stability data from an exploratory investigation at Mach number 4.06 of an airplane configuration having a wing of trapezoidal plan form

Author:	Dunning, Robert W
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55A21
Link:	https://digital.library.unt.edu/ark:/67531/metadc61313/