This paper focuses on using a genetic algorithm to optimise composite scarf repairs subject to tensile loading by minimisng the normalised shear stress in the adhesive. Several parameters are modified to investigate their role in the effectiveness of the optimisation, including constraints to the optimised stacking sequence to increase the practicality of the design. These include enforcing a symmetric and stiffness-matched optimised layup to the parent structure. The studies show that additional constraints do reduce the effectiveness of the optimisation; but still provide adequate reduction in the maximum normalised adhesive shear stress
Repair involving composite patches are widely used in the aerospace industry as they allow for exten...
[Departement_IRSTEA]DS [TR1_IRSTEA]METHODO / MODELIXInternational audienceThis paper describes the o...
This paper addresses the optimisation of forming in manufacturing of composites. A simplified finit...
Bonded scarf repairs are used in composite structures when high strength recovery is needed or when ...
Scarf repairs of aerospace composite structures are today’s preferred technology. It is known that t...
Mechanics of the composite repair under tensile loading with and without overlay plies was examined ...
This paper presents an analytical method to optimise the profile of the scarf joint between dissimil...
Scarf repairs are the preferred method of repairing thick composite structures, especially when exte...
Scarf repairs are the preferred method of repairing composite structures, especially when externally...
An optimal design algorithm was used to determine the repair fiber angles that minimize the stress i...
Adhesive bonding offers a better load transfer between adherends, for the assembly and repair of com...
This paper presents a draping optimisation scheme based on the integration of a commercial kinemati...
Flush repairs to military aircraft are expected to become more prevalent as more thick skin composit...
Current repair techniques require the repair material to be identical to the parent structure in ply...
Bonded scarf repairs are used in composite structures when high strength recovery is needed or when ...
Repair involving composite patches are widely used in the aerospace industry as they allow for exten...
[Departement_IRSTEA]DS [TR1_IRSTEA]METHODO / MODELIXInternational audienceThis paper describes the o...
This paper addresses the optimisation of forming in manufacturing of composites. A simplified finit...
Bonded scarf repairs are used in composite structures when high strength recovery is needed or when ...
Scarf repairs of aerospace composite structures are today’s preferred technology. It is known that t...
Mechanics of the composite repair under tensile loading with and without overlay plies was examined ...
This paper presents an analytical method to optimise the profile of the scarf joint between dissimil...
Scarf repairs are the preferred method of repairing thick composite structures, especially when exte...
Scarf repairs are the preferred method of repairing composite structures, especially when externally...
An optimal design algorithm was used to determine the repair fiber angles that minimize the stress i...
Adhesive bonding offers a better load transfer between adherends, for the assembly and repair of com...
This paper presents a draping optimisation scheme based on the integration of a commercial kinemati...
Flush repairs to military aircraft are expected to become more prevalent as more thick skin composit...
Current repair techniques require the repair material to be identical to the parent structure in ply...
Bonded scarf repairs are used in composite structures when high strength recovery is needed or when ...
Repair involving composite patches are widely used in the aerospace industry as they allow for exten...
[Departement_IRSTEA]DS [TR1_IRSTEA]METHODO / MODELIXInternational audienceThis paper describes the o...
This paper addresses the optimisation of forming in manufacturing of composites. A simplified finit...