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Effect of propeller location and flap deflection on the aerodynamic characteristics of a wing-propeller combination for angles of attack from 0 degrees to 80 degrees
Author:
Newsom, William A , Jr
Year:
1957
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3917
Link:
https://digital.library.unt.edu/ark:/67531/metadc56577/
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