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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