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The effect of control stiffness and forward speed on the flutter of a 1/10-scale dynamic model of a two-blade jet-driven helicopter rotor
Author:
Brooks, George W.
Year:
1955
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3376
Link:
https://digital.library.unt.edu/ark:/67531/metadc56248/
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