The Effects of the Addition of Small Fuselage-Mounted Fins on the Static Directional Stability Characteristics of a Model of a 45 Degree Swept-Wing Airplane at Angles of Attack up to 15.3 degrees at a Mach Number of 2.01

Author: Spearman, M. Leroy
Additional Authors: Robinson, Ross B.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L56D16a
Link: https://digital.library.unt.edu/ark:/67531/metadc62788/

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