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Impact resistance of current design composite fan blades tested under short-haul operating conditionsBoron/epoxy and graphite/epoxy composite blades were impacted in a rotating whirligig facility with conditions closely simulating those which might be experienced by a STOL engine impacted with various foreign objects. The tip speed of the rotating blades was 800 feet per second. The blades were impacted with simulated birds, real birds, ice balls, and gravel. The results of composite blade impact tests were compared with a titanium blade tested under similar conditions. Neither composite material indicated a clear superiority over the other. Blades made from both composite materials showed more damage than the titanium blades.
Document ID
19740010559
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Steinhagen, C. A.
(General Electric Co. Evendale, OH, United States)
Salemme, C. T.
(General Electric Co. Evendale, OH, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1973
Subject Category
Aircraft
Report/Patent Number
R74AEG219
NASA-CR-134533
Report Number: R74AEG219
Report Number: NASA-CR-134533
Accession Number
74N18672
Funding Number(s)
CONTRACT_GRANT: NAS3-16777
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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