Comparison of effect of a turbojet engine and three cold-flow configurations on the stability of a full-scale supersonicle inlet

Author: Musial, Norman T
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E56K23
Link: https://digital.library.unt.edu/ark:/67531/metadc63297/

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