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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