Damping in Roll of Rectangular Wings of Several Aspect Ratios and Naca 65a-Series Airfoil Sections of Several Thickness Ratios at Transonic and Supersonic Speeds as Determined With Rocket-Powered Models

Author: Edmondson, James L.
Year: 1950
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L50E26
Link: https://digital.library.unt.edu/ark:/67531/metadc64676/

< New search