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Task 4 stage data and performance report for casing treatment investigations. Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 1Test description and results for high Mach number transonic fan stages to determine range and distortion tolerance for various rotor tip casing treatment configurations
Document ID
19710015984
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tesch, W. A. (General Electric Co. Cincinnati, OH, United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1971
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-72862
GE-R71-AEG-149-VOL-1
Report Number: NASA-CR-72862
Report Number: GE-R71-AEG-149-VOL-1
Accession Number
71N25460
Funding Number(s)
CONTRACT_GRANT: NAS3-11157
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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