1. Elder D, Thomson R, Scott ML. Comparison of composite damage predictions between a 2D, 3D LS-Dyna simulation and experimental results for a low speed impact event. In: Proceedings of Tenth Australian International Aerospace Congress (AIAC-10), Brisbane, Australia, July 29–August 1 2003
2. Rajbhandari SP. Parametric finite element modelling of monolithic composite structures for impact damage. Master of Engineering thesis, Royal Melbourne Institute of Technology, Melbourne, Australia; 2003
3. Yap JWH, Scott ML, Hachenberg D, Baaran J, Rolfes R. Composite stiffened panels impact damage simulation and parametric studies. In: Proceedings of Tenth Australian International Aerospace Congress (AIAC-10), Brisbane, Australia, July 29–August 1 2003
4. Fleming DC. Delamination modelling of composites for improved crash analysis. National Aeronautics and Space Administration, Langley Research Center, Hampton, Virginia, USA, NASA/CR-1999-209725; 1999
5. Davidson BD. A predictive methodology for delamination growth in laminated composites. Part 1. Theoretical development and preliminary experimental results. US Department of Transport, Federal Aviation Administration, DOT/FAA/AR-97/87, Springfield, Virginia; 1998