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Detail Calculations of the Estimated Shift in Stick-Fixed Neutral Point Due to the Windmilling Propeller and to the Fuselage of the Republic XF-12 Airplane
Author:
White, M. D.
Year:
1944
Document Type:
N/A
Report Number:
NACA-CMR-L4J16
Link:
https://digital.library.unt.edu/ark:/67531/metadc64936/
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