Effect of a Rapid Blade-Pitch Increase on the Thrust and Induced-Velocity Response of a Full-Scale Helicopter Rotor

Author: Carpenter, Paul J.
Year: 1953
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-3044
Link: https://digital.library.unt.edu/ark:/67531/metadc56734/

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