Damping in Roll of Straight and 45 Degree Swept Wings of Various Taper Ratios Determined at High Subsonic, Transonic, and Supersonic Speeds With Rocket-Powered Models

Author:	Sanders, E. Claude, Jr.
Year:	1951
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L51H14
Link:	https://digital.library.unt.edu/ark:/67531/metadc59032/