Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by a free-oscillation method

Author: Tuovila, W J
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L56A26A
Link: https://digital.library.unt.edu/ark:/67531/metadc62334/

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