An Experimental Investigation of Two-Dimensional, Supersonic Cascade-Type Inlets at a Mach Number of 3.11

Author: Óffenhartz, Edward
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L54E17
Link: https://digital.library.unt.edu/ark:/67531/metadc60123/

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