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A Preliminary Investigation of the Pressure Recovery of Several Two-Dimensional Supersonic Inlets at Mach Number of 2.01
Author:
Comenzo, Raymond J.
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L54D14
Link:
https://digital.library.unt.edu/ark:/67531/metadc60464/
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