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Mechanical properties of the fiberglass prepreg system used for the National Transonic Facility replacement blade setThe results are presented of mechanical and physical properties characterization testing for the fiber glass prepreg system used to fabricate 15 of the replacement set of 25 fan blades for the National Transonic Facility. The fan blades were fabricated to be identical to the original blade set with the exception that the 7576 style E glass cloth used for the replacement set has a different surface finish than the original 7576 cloth. The 7781 E glass cloth and resin system were unchanged. The data are presented for elevated, room, and cryogenic temperatures. The results are compared with data from the original blade set and evaluated against selected structural design criteria. Test experience is described along with recommendations for future testing of these materials if required.
Document ID
19910008807
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Young, Clarence P., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Wallace, John W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1991
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-TM-102756
NAS 1.15:102756
Accession Number
91N18120
Funding Number(s)
PROJECT: RTOP 505-59-85-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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