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Investigation of a high-pressure-ratio eight-stage axial-flow research compressor with two transonic inlet stages I : aerodynamic design
Author:
Voit, Charles H
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E53I24
Link:
https://digital.library.unt.edu/ark:/67531/metadc59882/
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