Crack-tip force method for computing energy release rate in delaminated plates

Composite Structures

Volumn 55, Issue 4, 2002, Pages 429-434

  Park, Oung ^a   Sankar, Bhavani V ^a  

^a UNIVERSITY OF FLORIDA   (United States)

Author keywords

Composite laminates; Crack tip force method; Delamination; Energy release rate; Laminated plates; Virtual crack closure technique

Indexed keywords

CANTILEVER BEAMS; COMPUTATIONAL METHODS; CRACKS; DELAMINATION; FINITE ELEMENT METHOD; LOADS (FORCES); STRAIN RATE;

CRACK-TIP FORCE METHODS (CTFM);

PLATES (STRUCTURAL COMPONENTS);

COMPUTER SIMULATION; CRACKING; DELAMINATION; ENERGY; LAMINATE;

EID: 0036500251     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(01)00170-2     Document Type: Article

References (9)

1. Dynamic delamination propagation in composite beams
2. A double-plate finite-element model for the impact-induced delamination problem
3. A simplified improved beam analysis of the DCB specimen
4. A plate finite element for modeling delaminations
5. Estimating dynamic stress intensity factors in a length-wise cracked beam using remote data
6. A finite element for modeling delaminations in composite beams
7. Three-dimensional elastic analysis of a composite double cantilever beam specimen
8. Point-wise energy release rate in delaminated plates