Investigation of Downwash, Sidewash, and Mach Number Distribution Behind a Rectangular Wing at a Mach Number of 2.41

Author: Adamson, David
Year: 1950
Document Type: N/A
Series: NACA Technical Reports
Report Number: NACA-TR-1340
Link: https://digital.library.unt.edu/ark:/67531/metadc60746/

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