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Evaluation of range and distortion tolerance for high Mach number transonic fan stages, volume 1 Final reportPerformance tests of single stage, transonic compressor for advanced aircraft
Document ID
19710023725
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bilwakesh, K. R. (General Electric Co. Cincinnati, OH, United States)
Doyle, V. L. (General Electric Co. Cincinnati, OH, United States)
Koch, C. C. (General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1971
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-72806
GE-R71-AEG-133-VOL-1
Report Number: NASA-CR-72806
Report Number: GE-R71-AEG-133-VOL-1
Accession Number
71N33201
Funding Number(s)
CONTRACT_GRANT: NAS3-11157
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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