The Effect of a Simulated Propeller Slipstream on the Aerodynamic Characteristics of an Unswept Wing Panel With and Without Nacelles at Mach Numbers From 0.30 to 0.86

Author: Jordan, Gareth H.
Year: 1952
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-2776
Link: https://digital.library.unt.edu/ark:/67531/metadc56514/

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