Searched for: department%3A%22Aerospace%255C%252BStructures%255C%252B%2526%255C%252BMaterials%22
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document
Abouhamzeh, M. (author), Sinke, J. (author), Benedictus, R. (author)
Distortions and residual stresses are predicted in Fibre Metal Laminates (FMLs) under large deformations. A new modelling procedure is presented for small and large deformation analysis of thermo-viscoelastic problems of orthotropic materials. The material model is implemented in a finite element package which can be used for cure and/or...
journal article 2019
document
Müller, B. (author), Teixeira De Freitas, S. (author), Sinke, J. (author)
The development of fiber metal laminates to multi-functional materials by embedding heater elements in the laminate extends their field of application. Fiber metal laminates with embedded heater elements are likely to be used for the de- and anti-icing of leading edges in aircraft as they combine structural and heating functions. Hence, those...
conference paper 2015
document
Müller, B. (author), Teixeira de Freitas, S. (author), Sinke, J. (author)
The development of fiber metal laminates to multi-functional materials by embedding heater elements in the laminate extends their field of application. Fiber metal laminates with embedded heater elements are likely to be used for the de- and anti-icing of leading edges in aircraft as they combine structural and heating functions. Hence, those...
conference paper 2015
document
Anisimov, A. (author), Muller, B. (author), Sinke, J. (author), Groves, R.M. (author)
The development of smart materials for embedding in aerospace composites provides enhanced functionality for future aircraft structures. Critical flight conditions like icing of the leading edges can affect the aircraft functionality and controllability. Hence, anti-icing and de-icing capabilities are used. In case of leading edges made of fibre...
conference paper 2015
document
Plokker, H.M. (author)
The fatigue life of an aircraft is dependent on the loads of the aircraft service spectrum. Due to the variable nature of the load spectrum, fatigue crack growth is accelerated and decelerated by interaction effects. Interaction effects, like crack closure, make an accurate prediction of the fatigue life challenging. The material GLARE, a...
master thesis 2005
Searched for: department%3A%22Aerospace%255C%252BStructures%255C%252B%2526%255C%252BMaterials%22
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