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Room Temperature and Elevated Temperature Composite Sandwich Joint TestingTesting of composite sandwich joint elements has been completed to verify the strength capacity of joints designed to carry specified running loads representative of a high speed civil transport wing. Static tension testing at both room and an elevated temperature of 350 F and fatigue testing at room temperature were conducted to determine strength capacity, fatigue life, and failure modes. Static tension test results yielded failure loads above the design loads for the room temperature tests, confirming the ability of the joint concepts tested to carry their design loads. However, strength reductions as large as 30% were observed at the elevated test temperature, where all failure loads were below the room temperature design loads for the specific joint designs tested. Fatigue testing resulted in lower than predicted fatigue lives.
Document ID
19990004379
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Walker, Sandra P.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1998
Subject Category
Nonmetallic Materials
Report/Patent Number
L-17746
NAS 1.15:208742
NASA/TM-1998-208742
Report Number: L-17746
Report Number: NAS 1.15:208742
Report Number: NASA/TM-1998-208742
Funding Number(s)
PROJECT: RTOP 537-06-34-20
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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