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Theoretical and Experimental Analysis of Low-Drag Supersonic Inlets Having a Circular Cross Section and a Central Body at Mach Numbers of 3.30, 2.75, and 2.45
Author:
Ferri, Antonio
Year:
1948
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L8H13
Link:
https://digital.library.unt.edu/ark:/67531/metadc57993/
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