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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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