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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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