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Performance of Axial-Flow Supersonic Compressor of XJ55-FF-1 Turbojet Engine 2 - Performance of Inlet Guide Vanes as Separate Component
Author:
Graham, Robert C.
Year:
1949
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-SE9E03
Link:
https://digital.library.unt.edu/ark:/67531/metadc65369/
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