Add to ORKGOut-of-plane loading on composite T-joints may result in catastrophic failure of the structure. In this article a numerical parameter study on the mechanical response of composite T-joints subjected to out-of-plane tensile loading is performed using LS-DYNA. The influence of both, material parameters (mode I fracture toughness and stiffness of the filler material) and geometric constraints (curvature, overlap length) on the strength of the joint is quantified. Suggestions for an optimal T-Joint design are made
Composites are increasingly being used in aerospace, automotive and other industries. The T-joint (a...
An experimental and numerical study of the failure behaviour of composite T-joints under quasi-stati...
Primary aircraft structures benefit from the weight savings potential of carbon fiber reinforced pla...
An experimental and numerical study of the failure behaviour of composite T-joints under quasistatic...
In this work, a T-joint structure made of woven fabric carbon/epoxy composite has been numerically i...
In this work, a T-joint structure made of woven fabric carbon/epoxy composite has been numerically i...
This study assesses three different and novel design approaches to increase the failure stress and e...
The composite T-joint, a typical structural element, is widely used in the fields of aerospace due t...
Nonstandard tests are necessary for analyses and verification of new developed structural and techno...
Fibre reinforced polymers are progressively substituting metallic materials in many aerospace struct...
Composite sandwich structures are widely used in many fields. T-joint plays a significant role in th...
peer-reviewedThe full text of this article will not be available in ULIR until the embargo expires ...
This paper presents a study on thermoplastic single-lap double rivet joints (SLDJ) with and without ...
This study presents an investigation into the failure mechanism and strength improvement of a sandwi...
This paper reports on a series of tensile pull off tests on Composite T-joints as part of a comprehe...
Composites are increasingly being used in aerospace, automotive and other industries. The T-joint (a...
An experimental and numerical study of the failure behaviour of composite T-joints under quasi-stati...
Primary aircraft structures benefit from the weight savings potential of carbon fiber reinforced pla...
An experimental and numerical study of the failure behaviour of composite T-joints under quasistatic...
In this work, a T-joint structure made of woven fabric carbon/epoxy composite has been numerically i...
In this work, a T-joint structure made of woven fabric carbon/epoxy composite has been numerically i...
This study assesses three different and novel design approaches to increase the failure stress and e...
The composite T-joint, a typical structural element, is widely used in the fields of aerospace due t...
Nonstandard tests are necessary for analyses and verification of new developed structural and techno...
Fibre reinforced polymers are progressively substituting metallic materials in many aerospace struct...
Composite sandwich structures are widely used in many fields. T-joint plays a significant role in th...
peer-reviewedThe full text of this article will not be available in ULIR until the embargo expires ...
This paper presents a study on thermoplastic single-lap double rivet joints (SLDJ) with and without ...
This study presents an investigation into the failure mechanism and strength improvement of a sandwi...
This paper reports on a series of tensile pull off tests on Composite T-joints as part of a comprehe...
Composites are increasingly being used in aerospace, automotive and other industries. The T-joint (a...
An experimental and numerical study of the failure behaviour of composite T-joints under quasi-stati...
Primary aircraft structures benefit from the weight savings potential of carbon fiber reinforced pla...