A Preliminary Theoretical Study of Helicopter-Blade Flutter Involving Dependence Upon Coning Angle and Pitch Setting

Author: Coleman, Robert P.
Year: 1946
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-692, NACA-MR-L6G12
Link: https://digital.library.unt.edu/ark:/67531/metadc61843/

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