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Experimental evaluation of a honeycomb rotor shroud configuration to improve the stall margin of a 0.5 hub-tip ratio single-stage compressor. Volume 2 - Data supplementFlow distribution data for solid and honeycomb rotor shrouds to improve stall margin of 0.5 hub tip ratio single stage compressor
Document ID
19710005854
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Oscarson, R. P. (Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Wright, D. L. (Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
August 6, 2013
Publication Date
December 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
PWA-FR-4163
NASA-CR-72809
Report Number: PWA-FR-4163
Report Number: NASA-CR-72809
Accession Number
71N15329
Funding Number(s)
CONTRACT_GRANT: NAS3-11158
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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