ABSTRACT: With the wide application of fiber-reinforced composite materials in aero-structures, robotic arms, and mechanical parts, the design of composite joints has become a very important research area. In this article, linear finite element analyses in which the pin of the composite joint is assumed to be a frictionless rigid body are performed and the failure load of the mechanically fastened composite joint is predicted by the failure area index (FAI) method. From these analyses, it has been found that the FAI method can predict the failure loads of composite joints to within 20.1%. KEY WORDS: composite joint, failure criterion, joint strength
This paper describes progress towards developing design guidelines for a number of composite bonded ...
A method is presented for predicting the failure strength and failure mode of pin-loaded holes in fi...
Failure analysis of bonded composite joints is essential to the design of modern aerospace vehicles ...
ABSTRACT: With the wide application of fiber-reinforced composite material in aero-structures and me...
A method is presented for predicting the failure strength and failure mode of mechanically fastened ...
Adhesively bonded composite (ABC) joints used in the composite structures are modeled using 1D and 2...
ABSTRACT: This paper predicted the strength of mechanical joint of composites under bending load by ...
Application of an all-composite ? joint as a structural connector for integrated aircraft structures...
As these composites have become more popular, composite joint design has become a very important res...
This thesis describes progression towards developing an enhanced design methodology for laminated co...
ABSTRACT: A two-dimensional progressive failure analysis is conducted to predict the failure loads a...
International audienceComposite materials are widely used by aircraft manufacturers because of their...
A new set of failure criteria to predict composite failure in single lap bolted joints is proposed. ...
International audienceComposite materials are widely used by aircraft manufacturers because of their...
ABSTRACT: The aim of this research is to investigate the pin/hole contact stress of a composite lami...
This paper describes progress towards developing design guidelines for a number of composite bonded ...
A method is presented for predicting the failure strength and failure mode of pin-loaded holes in fi...
Failure analysis of bonded composite joints is essential to the design of modern aerospace vehicles ...
ABSTRACT: With the wide application of fiber-reinforced composite material in aero-structures and me...
A method is presented for predicting the failure strength and failure mode of mechanically fastened ...
Adhesively bonded composite (ABC) joints used in the composite structures are modeled using 1D and 2...
ABSTRACT: This paper predicted the strength of mechanical joint of composites under bending load by ...
Application of an all-composite ? joint as a structural connector for integrated aircraft structures...
As these composites have become more popular, composite joint design has become a very important res...
This thesis describes progression towards developing an enhanced design methodology for laminated co...
ABSTRACT: A two-dimensional progressive failure analysis is conducted to predict the failure loads a...
International audienceComposite materials are widely used by aircraft manufacturers because of their...
A new set of failure criteria to predict composite failure in single lap bolted joints is proposed. ...
International audienceComposite materials are widely used by aircraft manufacturers because of their...
ABSTRACT: The aim of this research is to investigate the pin/hole contact stress of a composite lami...
This paper describes progress towards developing design guidelines for a number of composite bonded ...
A method is presented for predicting the failure strength and failure mode of pin-loaded holes in fi...
Failure analysis of bonded composite joints is essential to the design of modern aerospace vehicles ...