Empirical Relation Between Induced Velocity, Thrust, and Rate of Descent of a Helicopter Rotor as Determined by Wind-Tunnel Tests on Four Model Rotors

Author: Castles, Walter, Jr.
Year: 1951
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-2474
Link: https://digital.library.unt.edu/ark:/67531/metadc55823/

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