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Preliminary investigation of a rectangular supersonic scoop inlet with swept sides designed for low drag at a Mach number of 2.7
Author:
Comenzo, Raymond J.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L52J02
Link:
https://digital.library.unt.edu/ark:/67531/metadc59426/
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