The Effects of Compressibility on the Upwash at the Propeller Planes of a Four-Engine Tractor Airplane Configuration Having a Wing With 40 Degrees of Sweepback and an Aspect Ratio of 10

Author: Lopez, Armando E.
Year: 1956
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-3675
Link: https://digital.library.unt.edu/ark:/67531/metadc56820/

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