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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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