The role of the resin fillet in the delamination of honeycomb sandwich structures

Composites Science and Technology

Volumn 62, Issue 14, 2002, Pages 1811-1819

  Okada, Ryo ^a   Kortschot, M T ^a  

^a UNIVERSITY OF TORONTO   (Canada)

Author keywords

A. Layered structures; B. Plastic deformation; C. Delamination; C. Laminates; Honeycomb

Indexed keywords

DELAMINATION; FRACTURE; HONEYCOMB STRUCTURES; LOADS (FORCES); PEELING; RESINS;

RESIDUAL AREA FRACTION; SINGLE MASTER CURVE;

COMPOSITE MATERIALS;

LAMINATE;

EID: 0036837185     PISSN: 02663538     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0266-3538(02)00099-4     Document Type: Article

References (16)

1. The adhesive-honeycomb relationship
2. A theoretical approach to the deformation of honeycomb based composite materials
3. Strength of sandwich beams with interface debondings
4. Evaluation of a high-temperature adhesive for aerospace structural bonding
5. Test technique for assessing core-skin adhesion in composite sandwich structures
6. Interfacial fracture of sandwich beams
7. Effects of processing variables on mechanical properties of nonmetallic sandwich structures
8. Self-adhesive honeycomb prepreg systems for secondary structural applications
9. Eddy current testing of brazed titanium honeycomb
10. Structural analysis of the adhesive bond in a honeycomb core sandwich panel
11. Analysis of debonding fracture in a sandwich plate with hexagonal core
12. A computational fracture mechanics approach for the analysis of facesheet-from-core disbond of honeycomb core sandwich panels
13. The effect of weave pattern and crack propagation direction on Mode I delamination resistance of woven glass and carbon composites
14. Effect of interfacial properties and weave structuré on Mode I interlaminar fracture behaviour of glass satin woven fabric composites