Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8

Author: Sears, R. I.
Year: 1955
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-3218
Link: https://digital.library.unt.edu/ark:/67531/metadc57405/

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