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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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