Progressive failure analyses of compression-loaded composite curved panels with and without cutouts

Composite Structures

Volumn 65, Issue 2, 2004, Pages 143-155

  Ambur, Damodar R ^a   Jaunky, Navin ^b   Hilburger, Mark ^a   Dávila, Carlos G ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NATIONAL INSTITUTE OF AEROSPACE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; COMPACTION; COMPUTATIONAL GEOMETRY; DEGRADATION; FAILURE ANALYSIS; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; STRUCTURAL PANELS;

COMPOSITE CURVED PANELS; COMPRESSION-LOADED COMPOSITE MATERIALS; FIBER-MATRIX SHEAR; MATRIX CRACKING;

COMPOSITE MATERIALS;

COMPOSITE PROPERTY; COMPRESSION; LOADING; STRUCTURAL ANALYSIS;

EID: 2642531801     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(03)00184-3     Document Type: Article

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