Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Mechanical EngineeringIn this work, the effect of different parameters, including stacking sequence, part thickness, and tooling material, on distortion of flat panels was investigated. A Romer arm equipped with a laser scanner was used to obtain the maximum amount of distortion as well as the 3D pattern of distortion for each panel. Among the different stacking sequences, the maximum distortion was observed in the asymmetric and balanced panel, while the least distortion belonged to the symmetric and unbalanced one. Furthermore, thinner panels were more distorted than thicker panels with the same planar size and stacking sequences. This study showed that distortion o...
International audienceOut-of-plane deformation generally develops for laminate composites during aut...
The work presented herein aims to characterise the in-plane properties of cross-plied unidirectional...
Purpose: The purpose of this paper is to elucidate the effect of part thickness and build orientatio...
Click on the DOI link to access the article (may not be free.)To predict the final geometry of carbo...
This paper presents an original method in predicting the spring-back for composite aircraft structur...
This paper presents an original method in predicting the spring-back for composite aircraft structur...
A fast-cure carbon fiber/epoxy prepreg was thermoformed against a replicated automotive roof panel m...
Process distortions are still a challenge in composite manufacturing. In academia and in industry, c...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Mechanical Engineering.The...
Counteracting undesired manufacturing distortions of carbon-composite structures is still a challeng...
The effect of stacking sequence, specimen thickness, tooling material and curing cycle on process in...
This paper presents a non-linear finite element analysis (FEA) method to predict the spring-back def...
The residual stresses that develop within fibre-reinforced laminate composites during autoclave proc...
Thermoplastic composite materials are of great interest in aerospace structures due to their potenti...
High performance composites usually consist of continuous fibres and a thermoset matrix. A well-know...
International audienceOut-of-plane deformation generally develops for laminate composites during aut...
The work presented herein aims to characterise the in-plane properties of cross-plied unidirectional...
Purpose: The purpose of this paper is to elucidate the effect of part thickness and build orientatio...
Click on the DOI link to access the article (may not be free.)To predict the final geometry of carbo...
This paper presents an original method in predicting the spring-back for composite aircraft structur...
This paper presents an original method in predicting the spring-back for composite aircraft structur...
A fast-cure carbon fiber/epoxy prepreg was thermoformed against a replicated automotive roof panel m...
Process distortions are still a challenge in composite manufacturing. In academia and in industry, c...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Mechanical Engineering.The...
Counteracting undesired manufacturing distortions of carbon-composite structures is still a challeng...
The effect of stacking sequence, specimen thickness, tooling material and curing cycle on process in...
This paper presents a non-linear finite element analysis (FEA) method to predict the spring-back def...
The residual stresses that develop within fibre-reinforced laminate composites during autoclave proc...
Thermoplastic composite materials are of great interest in aerospace structures due to their potenti...
High performance composites usually consist of continuous fibres and a thermoset matrix. A well-know...
International audienceOut-of-plane deformation generally develops for laminate composites during aut...
The work presented herein aims to characterise the in-plane properties of cross-plied unidirectional...
Purpose: The purpose of this paper is to elucidate the effect of part thickness and build orientatio...