The Subsonic Lateral and Longitudinal Static Stability Characteristics Up to Large Angles of Sideslip for a Triangular-Wing Airplane Model Having a Ventral Fin

Author: Buell, Donald A.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A56H06
Link: https://digital.library.unt.edu/ark:/67531/metadc62873/

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