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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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