Analysis of Limitations Imposed on One-Spool Turboprop-Engine Designs by Compressors and Turbines at Flight Mach Numbers of 0.06, and 0.8

Author: Cavicchi, Richard H.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E56I05
Link: https://digital.library.unt.edu/ark:/67531/metadc62919/

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