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Approximate design method for high-solidity blade elements in compressors and turbines
Document ID
19930082974
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Stanitz, John D
Date Acquired
August 16, 2013
Publication Date
July 1, 1951
Report/Patent Number
NACA-TN-2408
Report Number: NACA-TN-2408
Accession Number
93R12264
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLOW - TURBINES
FLOW - CHANNELS, CURVED
FLOW - COMPRESSORS
FLOW - AIRFOILS - CASCADES
TURBINES - BLADES
COMPRESSORS - BLADES
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