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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