Effect of Mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing

Author: Lindsey, W. F.
Year: 1944
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-75, NACA-CB-L4E29
Link: https://digital.library.unt.edu/ark:/67531/metadc62406/

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