Experimental Investigation at High Subsonic Speeds to Determine the Rolling-Stability Derivatives of Three Wing-Fuselage Configurations

Author: Sleeman, William C., Jr.
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L54H11
Link: https://digital.library.unt.edu/ark:/67531/metadc60656/

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