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Prediction of stiffener-skin separation in composite panelsA methodology was developed to predict the failure of stiffened composite panels by stiffener-skin separation. The methodology is applicable to curved or flat panels under combined uniaxial compression and in-plane shear loads. The analytical crux of the methodology are two different analysis packages: PACL1, which predicts the stress and displacement fields in a stiffened postbuckled panel; and WEBSTER, which predicts the local interfacial (shear and normal) stresses at the skin and stiffener flange junction. PACL1 is a Rayleigh-Ritz analysis of curved composite panels loaded into a post-buckling range. WEBSTER is a two-dimensional elasticity analysis for the skin-stiffener interface. Results of the predictive methodology are given.
Document ID
19930021682
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kan, Han-Pin
(Northrop Corp. Hawthorne, CA, United States)
Mahler, Mary A.
(Northrop Corp. Hawthorne, CA, United States)
Deo, Ravi B.
(Northrop Corp. Hawthorne, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA. Langley Research Center, First NASA Advanced Composites Technology Conference, Part 2
Subject Category
Composite Materials
Accession Number
93N30871
Funding Number(s)
CONTRACT_GRANT: NAS1-18842
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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