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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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