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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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