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An experimental investigation of the zero-lift pressure distribution over a wedge airfoil in closed, slotted, and open-throat tunnels at transonic Mach numbers
Author:
Nelson, William J.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L52C18
Link:
https://digital.library.unt.edu/ark:/67531/metadc59247/
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