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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