High-order behavior of sandwich panels with a bilinear transversely flexible core

Composite Structures

Volumn 53, Issue 1, 2001, Pages 87-106

  Schwarts Givli, Hilla ^a   Frostig, Yeoshua ^a  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

SHEAR STRESS; STRESS ANALYSIS; STRESS RELAXATION; STRUCTURAL ANALYSIS; STRUCTURAL PANELS;

MATERIAL NONLINEARITIES;

SANDWICH STRUCTURES;

LOADING; MATHEMATICAL ANALYSIS; STRESS; THEORY;

EID: 0035399526     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(00)00181-1     Document Type: Article

References (19)

1. The static and impact elastic-plastic behavior of polymer composite sandwich beams
2. Elasto-plastic yield limits and deformation laws for transversely crushed honeycomb
3. Analysis of high strain compression of open-cell foams
4. The in-plane non-linear compression of regular honeycomb
5. On the response of a sandwich panel with a bilinear core
6. Deflection of carbon fiber/acrylic foam sandwich beams
7. Departures from classical beam theory in laminated sandwich and short beams
8. A high order theory for bending of sandwich beams with a flexible core
9. Behavior of delaminated sandwich beam with transverse flexible core-high order theory
10. Behavior of unidirectional sandwich panels with a multi-skin construction or a multi-layered core layout - A high order approach