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...
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...
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...
Benchmark Finite Element Simulations of Postbuckling Composite Stiffened Panels (2005)
Orifici, Adrian, Thomson, R., Gunnion, A.J., Degenhardt, Richard, Abramovich, H., Bayandor, J.
This paper outlines the CRC-ACS contribution to a software code benchmarking exercise as part of the European Commission Project COCOMAT investigating composite postbuckling stiffened panels....
A review of explicit finite element software for composite impact analysis (2005)
Nguyen, M, Elder, D, Bayandor, J, Thomson, R, Scott, M
As explicit finite element (FE) codes improve and advanced material models become available, such tools will find more widespread application within the aerospace industry, as `what-if simulations...
Damage assessment and monitoring of composite ship joints (2005)
Herszberg, I, Li, H, Dharmawan, F, Mouritz, A, Nguyen, M, Bayandor, J
This paper describes the research activities associated with the damage assessment of maritime structures. conducted within (he Cooperative Research Centre for Advanced Composite Structures, which...
Parametric optimisation of composite shell structures for an aircraft Krueger flap (2002)
Bayandor, J, Scott, M, Thomson, R
This paper details the conceptual design previous term optimisation next term of the configuration and previous term composite next term lay-ups used to replace the conventional honeycomb stiffened...