An analysis methodology for failure in postbuckling skin-stiffener interfaces (2008)
Orifici, Adrian, Thomson, R.S., Herszberg, I., Weller, T., Degenhardt, Richard, Bayandor, J.
Blade-stiffened structures have the potential to produce highly efficient structures, particularly when the large strength reserves available after structural buckling, in the postbuckling range, are...
An analysis tool for design and certification of postbuckling composite aerospace structures (2008)
Orifici, Adrian, Thomson, R.S., Degenhardt, Richard
An experimental and numerical investigation was performed into the damage mechanisms and failure loads in skinstiffener sections. In the experimental investigation, thin strips consisting of a skin...
Design and Analysis of Stiffened Composite Panels Including Postbuckling and Collapse (2008)
Degenhardt, Richard, Kling, Alexander, Rohwer, Klaus, Orifici, A., Thomson, R.S.
he European aircraft industry demands reduced development and operating costs, by 20% and 50% in the short and long term, respectively. Contributions to this aim are provided by the completed project...
Degradation investigation in a postbuckling composite stiffened fuselage Panel (2008)
Orifici, Adrian, Thomson, R.S., Degenhardt, Richard, Kling, Alexander, Rohwer, Klaus, Bayandor, J.
COCOMAT is a four-year project under the European Commission 6th Framework Programme that aims to exploit the large strength reserves of composite structures through a more accurate prediction of...
Development of a Finite Element Methodology for Modelling Mixed-Mode Delamination Growth (2007)
Orifici, Adrian, Thomson, R.S., Degenhardt, Richard, Büsing, S., Bayandor, J.
A critical failure mechanism for composite skin-stiffened structures in compression is separation of the skin and stiffener, which can be considered analogous to interlaminar cracking. This paper...
Orifici, Adrian, Thomson, R.S., Degenhardt, Richard, Bisagni, C., Bayandor, J.
Analysing the collapse of skin-stiffened structures requires capturing the critical phenomenon of skin-stiffener separation, which can be considered analogous to interlaminar cracking. This paper...
Design and Analysis of Stiffened Composite Panels Including Postbuckling and Collapse (2007)
Degenhardt, Richard, Kling, Alexander, Rohwer, Klaus, Orifici, A., Thomson, R.S.
The European aircraft industry demands reduced development and operating costs, by 20% and 50% in the short and long term, respectively. Contributions to this aim are provided by the completed...
Orifici, Adrian, Thomson, R.S., Degenhardt, Richard, Bisagni, C., Bayandor, J.
Analysing the collapse of skin-stiffened structures requires capturing the critical phenomenon of skin-stiffener separation, which can be considered analogous to interlaminar cracking. This paper...
Degradation investigation in a postbuckling composite stiffened fuselage panel (2005)
Orifici, Adrian, Thomson, R.S., Degenhardt, Richard, Kling, Alexander, Rohwer, Klaus, Bayandor, J.
The European Commission Project COCOMAT (Improved MATerial Exploitation at Safe Design of COmposite Airframe Structures by Accurate Simulation of COllapse) is a currently running four-year project...
Compression, flexure and shear properties of a sandwich composite containing defects (1999)
The mechanical properties of a sandwich composite containing interfacial cracks or impact damage are compared when loaded in edgewise compression, flexure or shear. The composite is made from glass...
Compression, flexure and shear properties of a sandwich composite containing defects (1999)
The mechanical properties of a sandwich composite containing interfacial cracks or impact damage are compared when loaded in edgewise compression, flexure or shear. The composite is made from glass...
Compression, flexure and shear properties of a sandwich composite containing defects (1999)
The mechanical properties of a sandwich composite containing interfacial cracks or impact damage are compared when loaded in edgewise compression, flexure or shear. The composite is made from glass...
Compression, flexure and shear properties of a sandwich composite containing defects (1999)
The mechanical properties of a sandwich composite containing interfacial cracks or impact damage are compared when loaded in edgewise compression, flexure or shear. The composite is made from glass...
Shear properties of a sandwich composite containing defects (1998)
Thomson, R.S., Shah Khan, M.Z., Mouritz, A.P.
This paper investigates the effects of interfacial crack size and impact damage size on the shear properties and failure mechanisms of a typical marine sandwich composite made from glass reinforced...
Shear properties of a sandwich composite containing defects (1998)
Thomson, R.S., Shah Khan, M.Z., Mouritz, A.P.
This paper investigates the effects of interfacial crack size and impact damage size on the shear properties and failure mechanisms of a typical marine sandwich composite made from glass reinforced...
Shear properties of a sandwich composite containing defects (1998)
Thomson, R.S., Shah Khan, M.Z., Mouritz, A.P.
This paper investigates the effects of interfacial crack size and impact damage size on the shear properties and failure mechanisms of a typical marine sandwich composite made from glass reinforced...
Shear properties of a sandwich composite containing defects (1998)
Thomson, R.S., Shah Khan, M.Z., Mouritz, A.P.
This paper investigates the effects of interfacial crack size and impact damage size on the shear properties and failure mechanisms of a typical marine sandwich composite made from glass reinforced...