Optimal scarf joint between unmatched adherends

International SAMPE Symposium and Exhibition (Proceedings)

Volumn 51, Issue , 2006, Pages

  Wang, Chun H ^a   Harman, Alex B ^a  

^a DEFENCE SCIENCE AND TECHNOLOGY ORGANISATION   (Australia)

Author keywords

Adhesive bonded joint; Composite repair; Finite element; Scarf

Indexed keywords

ADHESIVES; BONDING; COMPOSITE MATERIALS; JOINTS (STRUCTURAL COMPONENTS); REPAIR;

ADHESIVE BONDED JOINTS; COMPOSITE REPAIR;

FINITE ELEMENT METHOD;

EID: 34748912618     PISSN: 08910138     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Hart Smith, L.J., Adhesive-bonded scarf and stepped-lap joints. 1973, Mcdonnell-Douglas Corp., Long Beach, Calif., NASA-CR-112237
2. Harman, A. and Wang, C. Improved design methods for scarf repairs to highly strained composite aircraft structure, in ICCS. 2005. Monash University, Melbourne, Australia.
3. Erdogan, F. and Ratwani, M., Stress Distribution in Bonded Joints. Composite Materials, 1971. 5: p. 379-393.
4. Chester, R.J., Baker, A.A., Hugo, G.R., and Radtke, T.C., Scarf repairs to highly strained graphite/epoxy structure. International Journal of Adhesion and Adhesives, 1999. 19(2-3): p. 161-171.
5. Chalkley, P. and Van Den Berg, J., On obtaining design allowables for adhesives used in the bonded composite repair of aircraft. DSTO-TR-0608, 1998.