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Certification of damage tolerant composite structureA reliability based certification testing methodology for impact damage tolerant composite structure was developed. Cocured, adhesively bonded, and impact damaged composite static strength and fatigue life data were statistically analyzed to determine the influence of test parameters on the data scatter. The impact damage resistance and damage tolerance of various structural configurations were characterized through the analysis of an industry wide database of impact test results. Realistic impact damage certification requirements were proposed based on actual fleet aircraft data. The capabilities of available impact damage analysis methods were determined through correlation with experimental data. Probabilistic methods were developed to estimate the reliability of impact damaged composite structures.
Document ID
19920023336
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rapoff, Andrew J.
(McDonnell Aircraft Co. Saint Louis, MO, United States)
Dill, Harold D.
(McDonnell Aircraft Co. Saint Louis, MO, United States)
Sanger, Kenneth B.
(McDonnell Aircraft Co. Saint Louis, MO, United States)
Kautz, Edward F.
(Naval Air Development Center Warminster, PA., United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1990
Publication Information
Publication: NASA. Langley Research Center, Eighth DOD(NASA)FAA Conference on Fibrous Composites in Structural Design, Part 2
Subject Category
Composite Materials
Accession Number
92N32580
Funding Number(s)
CONTRACT_GRANT: N62269-87-C-0227
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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