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Blade end wall flows in compressorsA brief summary of previous work carried out on end wall flow phenomena is presented with major emphasis on annulus wall boundary layer.
Document ID
19760020145
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sitaram, N. (Pennsylvania State Univ. University Park, PA, United States)
Lakshminarayana, B. (Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 3, 2013
Publication Date
June 30, 1976
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-148310
Report Number: NASA-CR-148310
Accession Number
76N27233
Funding Number(s)
CONTRACT_GRANT: NSG-3032
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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