International audienceIn this study, a simple finite-element model is developed to predict the spring-in of Z-section composite parts made of carbon fiber/ epoxy resin manufactured with resin transfer molding process. The different mechanisms occurring during manufacturing and effective in the formation of residual stresses and shape distortions are implemented. They are mainly the thermal effect and the chemical shrinkage of the resin during the cross-linking polymerization reaction. A dedicated experimental procedure allowing separation of strains to cure shrinkage and thermal expansion is presented to characterize the resin cure shrinkage. Cure kinetic properties of the resin are determined with differential scanning calorimetry measurem...
Advanced fibre-reinforced thermoset polymers are primarily used in the aerospace industry for their ...
This paper presents an original method in predicting the spring-back for composite aircraft structur...
Thermal shrinkage in advanced composite manufacturing causes residual stress in a cylindrical anisot...
Process-induced distortion of composite structures often leads to a violation of tolerances, making ...
Process-induced total spring-in of corner-shaped composite parts manufactured via autoclave-forming ...
A three-step finite element model has been implemented to predict the spring-in of L-shaped parts. T...
International audienceProperties of resin and composite, especially anisotropic coefficients of ther...
Click on the DOI link to access the article (may not be free.)To predict the final geometry of carbo...
The angular deformation is key parameter in composite manufacturing for curvature surfaces. Process ...
High performance composites usually consist of continuous fibres and a thermoset matrix. A well-know...
ABSTRACT: Cure-dependent mechanical properties are used in finite element-based models to determine ...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Mechanical Engineering.The...
Continuous-fibre-reinforced thermoset laminates that are cured hot, exhibit deformations due to cure...
Cure-induced deformations are inevitable in pultruded composite profiles due to the peculiarities of...
Cure-induced deformations are inevitable in pultruded composite profiles due to the peculiarities of...
Advanced fibre-reinforced thermoset polymers are primarily used in the aerospace industry for their ...
This paper presents an original method in predicting the spring-back for composite aircraft structur...
Thermal shrinkage in advanced composite manufacturing causes residual stress in a cylindrical anisot...
Process-induced distortion of composite structures often leads to a violation of tolerances, making ...
Process-induced total spring-in of corner-shaped composite parts manufactured via autoclave-forming ...
A three-step finite element model has been implemented to predict the spring-in of L-shaped parts. T...
International audienceProperties of resin and composite, especially anisotropic coefficients of ther...
Click on the DOI link to access the article (may not be free.)To predict the final geometry of carbo...
The angular deformation is key parameter in composite manufacturing for curvature surfaces. Process ...
High performance composites usually consist of continuous fibres and a thermoset matrix. A well-know...
ABSTRACT: Cure-dependent mechanical properties are used in finite element-based models to determine ...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Mechanical Engineering.The...
Continuous-fibre-reinforced thermoset laminates that are cured hot, exhibit deformations due to cure...
Cure-induced deformations are inevitable in pultruded composite profiles due to the peculiarities of...
Cure-induced deformations are inevitable in pultruded composite profiles due to the peculiarities of...
Advanced fibre-reinforced thermoset polymers are primarily used in the aerospace industry for their ...
This paper presents an original method in predicting the spring-back for composite aircraft structur...
Thermal shrinkage in advanced composite manufacturing causes residual stress in a cylindrical anisot...