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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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