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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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