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Performance of an axial-flow compressor rotor designed for a pitch-section lift coefficient of 1.20
Author:
Herrig, L. Joseph
Year:
1947
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-1388
Link:
https://digital.library.unt.edu/ark:/67531/metadc55447/
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