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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
19830021461
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
September 4, 2013
Publication Date
March 1, 1983
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:84627
NASA-TM-84627
Report Number: NAS 1.15:84627
Report Number: NASA-TM-84627
Meeting Information
Meeting: Am. Helicopter Soc. Composite Struct. Specialist''s Conf.
Location: Philadelphia
Start Date: March 23, 1983
End Date: March 25, 1983
Accession Number
83N29732
Funding Number(s)
PROJECT: RTOP 534-03-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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