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Turning-angle design rules for constant-thickness circular-arc inlet guide vanes in axial annular flow
Document ID
19930082830
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lieblein, Seymour
Date Acquired
August 16, 2013
Publication Date
September 1, 1950
Report/Patent Number
NACA-TN-2179
Report Number: NACA-TN-2179
Accession Number
93R12120
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMPRESSORS, AXIAL
AIRFOILS, CIRCULAR - ARC
FLOW - VANES, GUIDE
VANES, GUIDE

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