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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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