Continuum Damage Mechanics of Composite Materials
The code development was led by Prof. Brian G. Falzon. The contritutors are Donadon, M.V., Faggiani, A., Chiu, L.N., Boman, R., Tan, W. Liu, H. et al.
Video guidelines:
- How to set up material properties for VUMAT: https://youtu.be/gTBC0OqdmYA
- How to run a subroutine in HPC without the need to install Intel Fortran Compiler: https://youtu.be/BiNk9z58-9M
If you use it for your research, please cite these references below:
[1] Donadon, M.V., Iannucci, L., Falzon, B.G., Hodgkinson, J.M. and de Almeida, S.F., 2008. A progressive failure model for composite laminates subjected to low velocity impact damage. Computers & Structures, 86(11-12), pp.1232-1252.
[2] Faggiani, A. and Falzon, B.G., 2010. Predicting low-velocity impact damage on a stiffened composite panel. Composites Part A: Applied Science and Manufacturing, 41(6), pp.737-749.
[3] Tan, W., Falzon, B.G., Chiu, L.N. and Price, M., 2015. Predicting low velocity impact damage and Compression-After-Impact (CAI) behaviour of composite laminates. Composites Part A: Applied Science and Manufacturing, 71, pp.212-226.
[4] Chiu, L.N., Falzon, B.G., Boman, R., Chen, B. and Yan, W., 2015. Finite element modelling of composite structures under crushing load. Composite Structures, 131, pp.215-228.