Damping in Yaw and Static Directional Stability of a Canard Airplane Model and of Several Models Having Fuselages of Relatively Flat Cross Section

Author: Johnson, Joseph L.
Year: 1950
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L50H30a
Link: https://digital.library.unt.edu/ark:/67531/metadc58654/

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