Theoretical Stability Derivatives of Thin Sweptback Wings Tapered to a Point with Sweptback or Sweptforward Trailing Edges for a Limited Range of Supersonic Speeds

Author:	Malvestuto, Frank S., Jr.
Year:	1948
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-971
Link:	https://digital.library.unt.edu/ark:/67531/metadc60305/