Low-speed measurement of static stability and damping derivatives of a 60 degree delta-wing model for angles of attack of 0 degrees to 90 degrees

Author:	Hewes, Donald E
Year:	1954
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L54G22a
Link:	https://digital.library.unt.edu/ark:/67531/metadc60807/