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Performance of a supersonic mixed-flow rotor with a swept leading edge and 0.52 inlet radius ratio
Author:
Goldstein, Arthur W.
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E53H27
Link:
https://digital.library.unt.edu/ark:/67531/metadc60020/
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