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Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor. Part 5 - Performance of plain casing insert configuration with distorted inlet flowOuter case bleeding or blowing effects on casing insert of single stage axial flow compressor with distorted inlet flow
Document ID
19690017195
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Koch, C. C. (General Electric Co. Lynn, MA, United States)
Date Acquired
August 5, 2013
Publication Date
May 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-54591
GE-R69AEG103
Report Number: NASA-CR-54591
Report Number: GE-R69AEG103
Accession Number
69N26573
Funding Number(s)
CONTRACT_GRANT: NAS3-7618
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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