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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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