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Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panelsThe structural efficiency of compression-loaded trapezoidal-corrugation sandwich and semisandwich composite panels is studied to determine their weight savings potential. Sandwich panels with two identical face sheets and a trapezoidal corrugated core between them and semisandwich panels with a corrugation attached to a single skin are considered. An optimization code is used to find the minimum weight designs for critical compressive load levels ranging from 3000 to 24,000 lb/in. Graphite-thermoplastic panels based on the optimal minimum weight designs were fabricated and tested. A finite element analysis of several test specimens was also conducted. The results of the optimization study, the finite element analysis, and the experiments are presented. The results of testing impact damage panels are also discussed.
Document ID
19930002435
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Jegley, Dawn C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1992
Subject Category
Composite Materials
Report/Patent Number
NAS 1.60:3264
NASA-TP-3264
L-17129
Report Number: NAS 1.60:3264
Report Number: NASA-TP-3264
Report Number: L-17129
Accession Number
93N11623
Funding Number(s)
PROJECT: RTOP 505-63-50-08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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