The aim of this research is to understand and analyse the behaviour of specimens used to measure fracture toughness in laminated composites when loaded at high displacement rates. Finite element (FE) analysis is used as a tool to investigate dynamic behaviour of rapidly loaded mode I intralaminar specimens and to investigate of the data reduction strategy. Finally, using knowledge from current literature and experience gathered from the FE analysis, an experimental test procedure for the measurement of intra-laminar fracture toughness at high loading rates is designed and evaluated. To gain confidence in the dynamic FE modelling the behaviour of a mode I interlaminar double-cantilever beam specimen loaded at high rates was analysed. The fin...
Automotive and aeronautical composite structures can be subjected to dynamic loading scenarios (e.g....
Automotive and aeronautical composite structures can be subjected to dynamic loading scenarios (e.g....
RQsumB: La relation entre la vitesse de deformation et la resistance F la rupture interlaminaire en ...
The aim of this research is to understand and analyse the behaviour of specimens used to measure fra...
n this work, the rate dependence of mode I interlaminar fracture toughness for two different materia...
Composite materials are often subjected to mechanical impact causing delamination. For quasi-static ...
The design of composite transportation structures with improved crashworthiness behaviour requires a...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.The ...
In this work, the rate dependence of mode I interlaminar fracture toughness for two different materi...
Abstract. The energy dissipation due to the failure of composites is of particular interest for cras...
In this work, the rate dependence of mode I interlaminar fracture toughness for two different materi...
In order to successfully model design-critical impact loading events on laminated composite structur...
This paper presents experimental investigations on the in-plane shear behaviour and intralaminar fib...
Paper presented to the 5th Annual Symposium on Graduate Research and Scholarly Projects (GRASP) held...
One of the major benefits of laminate composites reinforced with long fibers is the ability to orien...
Automotive and aeronautical composite structures can be subjected to dynamic loading scenarios (e.g....
Automotive and aeronautical composite structures can be subjected to dynamic loading scenarios (e.g....
RQsumB: La relation entre la vitesse de deformation et la resistance F la rupture interlaminaire en ...
The aim of this research is to understand and analyse the behaviour of specimens used to measure fra...
n this work, the rate dependence of mode I interlaminar fracture toughness for two different materia...
Composite materials are often subjected to mechanical impact causing delamination. For quasi-static ...
The design of composite transportation structures with improved crashworthiness behaviour requires a...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.The ...
In this work, the rate dependence of mode I interlaminar fracture toughness for two different materi...
Abstract. The energy dissipation due to the failure of composites is of particular interest for cras...
In this work, the rate dependence of mode I interlaminar fracture toughness for two different materi...
In order to successfully model design-critical impact loading events on laminated composite structur...
This paper presents experimental investigations on the in-plane shear behaviour and intralaminar fib...
Paper presented to the 5th Annual Symposium on Graduate Research and Scholarly Projects (GRASP) held...
One of the major benefits of laminate composites reinforced with long fibers is the ability to orien...
Automotive and aeronautical composite structures can be subjected to dynamic loading scenarios (e.g....
Automotive and aeronautical composite structures can be subjected to dynamic loading scenarios (e.g....
RQsumB: La relation entre la vitesse de deformation et la resistance F la rupture interlaminaire en ...