A FEM-based tool was developed for optimization of the geometry of an adhesive joint for implementation in a composite micro truss structure. A genetic algorithm was employed to optimize the adhesive fillet and adherend local end geometry towards a uniform state of strain in the adhesive layer. It was found that the peak maximum principal strain in the adhesive has been reduced up to 36.8 %. However, it was concluded that the optimized joint configurations are unfeasible for implementation in composite micro truss structures as the joint efficiency was estimated to be below 1.0 %.Aerospace EngineeringAerospace Structures & MaterialsStructural Integrity & Composit
The bonding strength of adhesive joints is influenced by many factors such as, the overlap, the bond...
ABSTRACT: A postbuckling analysis for composite stiffened structures is a repre-sentative nonlinear ...
Lightweight structures, especially trusses, have attracted a tremendous attention due to their exten...
This paper investigates the effect of the outer adherend geometry on the strength of an adhesively b...
In the context of lightweight structure design for the transportation and robotics industries, new t...
Parametric variation and optimisation using genetic algorithms employing single and multi-objective ...
The trend to use multi-material structures in automotive lightweight design leads to an increasing d...
The paper presents a mathematical model and method for solving a wide class of problems in topologic...
The potential to optimise the performance of microstructured joints based on mechanically interlocki...
This study presents three-dimensional free vibration and stress analyses of an adhesively bonded dou...
C Composite materials are most often used for lengthier and thin structures susceptible to buckle. T...
Adhesive bonded composite joints are traditionally difficult to model using finite element (FE) tech...
The design of a manipulator arm, which is built from a construction kit, is presented in this articl...
A novel concept for joining materials is presented which employs adhesive joints with interlocking b...
This study investigates the three-dimensional free vibration behaviour of an adhesively-bonded corne...
The bonding strength of adhesive joints is influenced by many factors such as, the overlap, the bond...
ABSTRACT: A postbuckling analysis for composite stiffened structures is a repre-sentative nonlinear ...
Lightweight structures, especially trusses, have attracted a tremendous attention due to their exten...
This paper investigates the effect of the outer adherend geometry on the strength of an adhesively b...
In the context of lightweight structure design for the transportation and robotics industries, new t...
Parametric variation and optimisation using genetic algorithms employing single and multi-objective ...
The trend to use multi-material structures in automotive lightweight design leads to an increasing d...
The paper presents a mathematical model and method for solving a wide class of problems in topologic...
The potential to optimise the performance of microstructured joints based on mechanically interlocki...
This study presents three-dimensional free vibration and stress analyses of an adhesively bonded dou...
C Composite materials are most often used for lengthier and thin structures susceptible to buckle. T...
Adhesive bonded composite joints are traditionally difficult to model using finite element (FE) tech...
The design of a manipulator arm, which is built from a construction kit, is presented in this articl...
A novel concept for joining materials is presented which employs adhesive joints with interlocking b...
This study investigates the three-dimensional free vibration behaviour of an adhesively-bonded corne...
The bonding strength of adhesive joints is influenced by many factors such as, the overlap, the bond...
ABSTRACT: A postbuckling analysis for composite stiffened structures is a repre-sentative nonlinear ...
Lightweight structures, especially trusses, have attracted a tremendous attention due to their exten...