Design and analysis of mechanically fastened composite joints and repairs

Engineering Analysis with Boundary Elements

Volumn 25, Issue 6, 2001, Pages 431-441

  Zhang, Jin Min ^a  

^a DSO NATIONAL LABORATORIES   (Singapore)

Author keywords

Anisotropy; Boundary element method; Doublers; Mechanical fastener

Indexed keywords

COMPOSITE JOINTS;

AIRCRAFT; BOUNDARY ELEMENT METHOD; FAILURE ANALYSIS; FIBER REINFORCED MATERIALS; JOINTS (STRUCTURAL COMPONENTS); STRESS ANALYSIS;

COMPOSITE STRUCTURES;

EID: 0035368407     PISSN: 09557997     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0955-7997(01)00049-2     Document Type: Article

References (22)

1. Failure of composite laminates containing pin-loaded holes-method of solution
2. Design of multiple row bolted composite joints under general in-plane loading
3. Strength analysis of mechanically fastened composite structures
4. Analysis of composite laminates with multiple fasteners
5. The analysis of mechanically fastened repairs and lap joints
6. Analysis of pin-loaded holes in composite laminates under combined bearing-bypass and shear loading
7. An analtical method for failure prediction of multi-fastener composite joints
8. Fastening and joining: Finite element and boundary element analysis. A bibliography (1992-1994)
9. The dual boundary element method, effective implementation for crack problem
10. Influence of the fastener flexibility on the prediction of load transfer and fatigue life for multi-row joints
11. Stress fracture criteria for laminated composites containing stress concentrations
12. Stress intensity factor for a cracked sheet with riveted and uniformly spaced sheet
13. Contact streses in bolted joints of composite laminates