Analysis of Effects of Inlet Pressure Losses on Performance of Axial-Flow Type Turbojet Engine

Author: Sanders, Newell D
Year: 1948
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E8J25b
Link: https://digital.library.unt.edu/ark:/67531/metadc62747/

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