Strength investigation of composite honeycomb structures after repair

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 22, Issue 3, 2001, Pages 270-273

  Wang, H ^a   Chen, X H ^a   Guo, X L ^a   Ren, M F ^a  

^a SHENYANG AIRCRAFT DESIGN AND RESEARCH INSTITUTE   (China)

Author keywords

Composite; Experimental validation; Finite element analyses; Honeycomb; Repair; Strength

Indexed keywords

FINITE ELEMENT METHOD; HONEYCOMB STRUCTURES; REPAIR; SANDWICH STRUCTURES; STIFFNESS; STRENGTH OF MATERIALS; STRESSES;

DAMAGES; FINITE ELEMENT STRESS ANALYSIS; SPECIMENS;

COMPOSITE MATERIALS;

EID: 0035342982     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (5)

1. The importance of failure mode identification in adhesive bonded aircraft structures and repairs
2. Failure mechanisms in bonded patch repaired structures
3. Bonded repairs in composite structures: A finite element approach
4. On the design of bonded patches for one-sided repair
5. Experimental investigation of composite bonded and/or bolted repairs using single lap joint design