Effect of dihedral change on the theoretical dynamic lateral response characteristics of a low-aspect-ratio straight-wing supersonic airplane

Author:	Heinle, Donovan R
Year:	1950
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A50H02
Link:	https://digital.library.unt.edu/ark:/67531/metadc58587/