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Hightip-speed, low-loading transonic fan stage. Part 2: Data compilationTests were conducted on a high-tip-speed low-loading transonic fan stage to determine the performance and inlet flow distortion tolerance of the design. Test data were recorded for overall and blade element performance with both uniform and distorted inlet flows. A tabular summary of the data and a representative selection of the computer data reduction sheets are presented.
Document ID
19740012328
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ware, T. C. (AiResearch Mfg. Co. Los Angeles, CA, United States)
Kobayashi, R. J. (AiResearch Mfg. Co. Los Angeles, CA, United States)
Jackson, R. J. (AiResearch Mfg. Co. Los Angeles, CA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1974
Subject Category
Propulsion Systems
Report/Patent Number
AIRESEARCH-73-9487
NASA-CR-121262
Report Number: AIRESEARCH-73-9487
Report Number: NASA-CR-121262
Accession Number
74N20441
Funding Number(s)
CONTRACT_GRANT: NAS3-13498
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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