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Ground test experience with large composite structures for commercial transportsThe initial ground test of each component resulted in structural failure at less than ultimate design loads. While such failures represent major program delays, the investigation and analysis of each failure revealed significant lessons for effective utilization of composites in primary structure. Foremost among these are secondary loads that produce through-the-thickness forces which may lead to serious weaknesses in an otherwise sound structural design. The sources, magnitude, and effects of secondary loads need to be thoroughly understood and accounted for by the designers of composite primary aircraft structures.
Document ID
19850039232
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bohon, H. L.
(NASA Langley Research Center Hampton, VA, United States)
Chapman, A. J., III
(NASA Langley Research Center Hampton, VA, United States)
Leybold, H. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: Composite structures
Location: Philadelphia, PA
Start Date: March 23, 1983
End Date: March 25, 1983
Accession Number
85A21383
Distribution Limits
Public
Copyright
Other

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