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Performance of NACA eight-stage axial-flow compressor designed on the basis of airfoil theory
Author:
Sinnette, John T
Additional Authors:
Schey, Oscar W
Year:
1943
Document Type:
N/A
Series:
NACA Technical Reports
Report Number:
NACA-TR-758
Link:
https://digital.library.unt.edu/ark:/67531/metadc60023/
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