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Effect of boundary-layer control and inlet lip shape on the performance of a twin-scoop air-induction system at Mach numbers from 0 to 1.9
Author:
Lazzeroni, Frank A.
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A55L02
Link:
https://digital.library.unt.edu/ark:/67531/metadc62032/
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