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Performance of an impulse-type supersonic-compressor rotor having a mean turning of 114 degrees
Author:
Goldberg, Theodore J.
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L56J01
Link:
https://digital.library.unt.edu/ark:/67531/metadc62862/
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