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Analysis of selected compression splice joint locations in a graphite-epoxy transport wing stub boxThree critical compression splice joint locations in a stitched graphite-epoxy transport wing stub box have been analyzed to determine their expected structural performance. The wing box is representative of a section of a commercial transport wing box and was designed and constructed by McDonnell Douglas Aerospace Company as part of the NASA Advanced Composites Technology (ACT) program. The results of the finite element analyses of the splice joints are presented. The analysis results indicate that failure will not occur in the splice joint regions for loads less than the Design Ultimate Load of the wing box.
Document ID
19960009063
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Jegley, Dawn C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1995
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-110170
NAS 1.15:110170
NIPS-95-06489
Accession Number
96N16229
Funding Number(s)
PROJECT: RTOP 510-02-12-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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