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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