Analysis of the distribution of thermal residual stresses in bonded composite repair of metallic aircraft structures

Computational Materials Science

Volumn 46, Issue 4, 2009, Pages 1023-1027

  Aminallah, L ^a,c   Achour, T ^b   Bachir Bouiadjra, B ^b   Serier, B ^b   Amrouche, A ^c   Feaugas, X ^d   Benssediq, N ^c  

^a UNIVERSITÉ DE MASCARA   (Algeria)

^b UNIVERSITY OF SIDI BEL ABBES   (Algeria)

^c UNIV LILLE   (France)

^d UNIVERSITÉ DE LA ROCHELLE   (France)

Author keywords

Adhesive; Bonded composite repair; Finite element method; Stress intensity factor; Thermal stresses

Indexed keywords

ADHESIVE CURING; ADHESIVE LAYERS; BONDED COMPOSITE REPAIR; BONDED COMPOSITE REPAIRS; COMPOSITE PATCHES; CRACKED PLATE; METALLIC AIRCRAFT STRUCTURES; THERMAL RESIDUAL STRESS;

AIRCRAFT; AIRCRAFT MANUFACTURE; AIRFRAMES; ASPHALT PAVEMENTS; CRACK TIPS; FIBER OPTIC SENSORS; PLATES (STRUCTURAL COMPONENTS); REPAIR; RESIDUAL STRESSES; STRESS INTENSITY FACTORS; THERMAL STRESS; THERMOELASTICITY;

FINITE ELEMENT METHOD;

EID: 70249104980     PISSN: 09270256     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.commatsci.2009.05.008     Document Type: Article

References (9)

1. A.A Baker, L.R.F. Rose, R. Jones, Advances in the Bonded Composite Repair of Metallic Aircraft Structures, Elsevier, 2002.
2. Wang Z., Xiao J., Jiang D., Zeng J., and Yang F. J. Reinf. Plas. Comp. 58 (2009) 587-599
3. Ratwani M. J. Eng. Mat. Tech. 100 (1978) 46-51
4. Wang C.H., Rose L.R.F., Callinan R., and Baker A.A. Int. J. Sol. Struct. 37 33 (2000) 4577-4599
5. A.M. Albat, Ph.D. Thesis, the University of British Columbia, Canada, 1993.
6. Sun A.T., Klug J., and Arendt C. AIAA Journal 34 2 (1996) 369-374
7. Djokic D., Johnston A., Rogers A., Lee-Sullivan P., and Mrad N. Compos. P.A: Appl. Sci. Manuf. 33 2 (2002) 277-288
8. D. Swenson, M. James, FRANC2D/L: A Crack Propagation Simulator for Plane Layered Structures, Version 1.4 User's guide, 1998.
9. Henshel R.D., and Shaw K.G. Int. J. Num. Met. Eng. 9 (1975) 495-507