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Optimized turning-vane design for an intake elbow of an axial-flow compressorElbow turning vane design for high recovery and Uniform distribution at exit of 90 deg intake elbow of axial flow compressor
Document ID
19660001042
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Pinckney, S. Z. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1965
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-3083
Accession Number
66N10331
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ELBOW
UNIFORM FLOW
AXIAL FLOW COMPRESSOR
VANE

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