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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