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Cooperative Research Centre for Advanced Composite Structures Ltd, 506 Lorimer St., Fishermans Bend, Victoria, 3207, Australia
Selected Publications (for more see the link Prof. Rodney S. Thomson):
R.S. Thomson, M.L. Scott, Modelling delaminations in postbuckling stiffened composite shear panels, Computational Mechanics, 26, 75-89, 2000.
J.W.H. Yap, M.L. Scott, R.S. Thomson, D. Hachenberg, The analysis of skin-to-stiffener debonding in composite aerospace structures, Composite Structures, 57, 425-435, 2002.
Sagar P. Rajbhandari, Murray L. Scott, Rodney S. Thomson and Dieter Hachenberg, “An approach to modeling and predicting impact damage in composite structures”, ICAS 2002 Congress
Elder D.J., Thomson R.S., Nguyen M.Q. and Scott M.L., “Review of delamination predictive methods for low speed impact of composite laminated composites”, Composite Structures, Vol. 66, 2004, pp. 677-683
R.S. Thomson and M.L. Scott, Int. Con. on Buckling and Postbuckling Behavior of Compos. Laminated Shell Struct. Eilat, Israel (2004).
J. W. H. Yap, R. S. Thomson, M. L. Scott, and D. Hachenberg, “Influence of post-buckling behaviour of composite stiffened panels on the damage criticality,” Comp. Struct., 66, 197–206 (2004).
Nguyen MQ, Jacombs SS, Thomson RS, Hachenberg D, Scott ML. Simulation of impact on sandwich structures. Compos Struct 2005;67:217–27.
Orifici AC, Thomson RS, Gunnion AJ, Degenhardt R, Abramovich H, Bayandor J. Benchmark finite element simulations of postbuckling composite stiffened panels. In: Proceedings of the Eleventh Australian International Aerospace Congress (AIAC-11), Melbourne, 13-17 March 2005
A. C. Orifici, R. S. Thomson, R. Degenhardt, C. Bisagni, and J. Bayandor, “Development of a degradation model for the collapse analysis of composite aerospace structures,” in: C. A. Mota Soares et al. (eds), Proc. of the 3rd Europ. Conf. on Computational Mechanics: Solids, Structures and Coupled Problems in Engineering, Lisbon, Portugal, 5–9 June (2006).
Orifici AC, Thomson RS, Degenhardt R and Bayandor J. Development of a finite element methodology for the collapse analysis of composite aerospace structures. ECCOMAS Thematic Conference on Mechanical Response of Composites, Porto, Portugal, 12-14 September, 2007.
Lee M, Kelly D, Orifici AC and Thomson RS. Postbuckling mode shapes of composite stiffened fuselage panels incorporating stochastic variables. 1st CEAS European Air and Space Conference, Berlin, Germany, 10-13 September, 2007.
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