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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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