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Mechanical properties of a fiberglass prepreg system at cryogenic and other temperaturesThe compressor driving the flow in the National Transonic Facility, which is nearing completion at the Langley Research Center, has 25 fiberglass blades. E-glass cloth with a pre-impregnated epoxy resin has been selected as the material for the fan blades because of its low cost, high damping, and fatigue resistance. A complete characterization is presented of this fan blade fiberglass system at temperatures of 367 K, room temperature, and 89 K. The characterization test results suggest that the material follows the general trends of metals and other glass-reinforced plastics at cryogenic temperatures. A slight diminution in strength was observed at the elevated temperature. The tests included the following: tensile, compression, fatigue, inplane shear, interlaminar shear, thermal expansion, creep, and thermal cycle.
Document ID
19820046564
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Klich, P. J.
(NASA Langley Research Center Hampton, VA, United States)
Cockrell, C. E.
(NASA Langley Research Center Systems Engineering Div., Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 82-0708
Meeting Information
Meeting: In: Structures, Structural Dynamics and Materials Conference
Location: New Orleans, LA
Start Date: May 10, 1982
End Date: May 12, 1982
Accession Number
82A30099
Distribution Limits
Public
Copyright
Other

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