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Experimental investigation of an axial-flow supersonic compressor having sharp leading-edge blades with an 8-percent mean thickness chord ratio
Document ID
19930088382
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Goldberg, Theodore J
Date Acquired
August 29, 2013
Publication Date
February 4, 1955
Report/Patent Number
NACA-RM-L54K16
Report Number: NACA-RM-L54K16
Accession Number
93R17672
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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