Flight Measurements of the Vibratory Stresses on a Propeller Designed for an Advance Ratio of 4.0 and a Mach Number of 0.82

Author: O'Bryan, Thomas C.
Year: 1958
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-4410
Link: https://digital.library.unt.edu/ark:/67531/metadc57462/

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