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Performance of NACA Eight-stage Axial-flow Compressor Designed on the Basis of Airfoil Theory
Document ID
19930093570
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
King, J Austin
Date Acquired
September 6, 2013
Publication Date
August 1, 1944
Report/Patent Number
NACA-WR-E-1
NACA-ACR-E4H18
Report Number: NACA-WR-E-1
Report Number: NACA-ACR-E4H18
Accession Number
93R22860
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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