Link to Index Page

Professor Wesley J. Cantwell

For more see the link: Prof. Wesley J. Cantwell

Aerospace Research and Innovation Center (ARIC)
Khalifa University of Science and Technology (KUST), Abu Dhabi, United Arab Emirates

Biography:
Professor Wesley Cantwell is the Director of the Aerospace Research and Innovation Center (ARIC) and a Professor of Aerospace Engineering at Khalifa University. He is also the Associate Dean for Research in the College of Engineering at Khalifa University. Prior to joining Khalifa, he was a Professor in the School of Engineering at the University of Liverpool (1994 – 2012) and a Research Scientist in the Department of Materials at the Ecole Polytechnique Federale de Lausanne (1985-1994) in Switzerland. He has also been a visiting scientist at Virginia Tech and the University of Kyushu, Japan. He received his MSc and PhD degrees in Aeronautical Engineering from Imperial College, London and his BSc in Aeronautical and Astronautical Engineering from the University of Southampton. Professor Wesley Cantwell’s research interests focus on the manufacture and testing of high-performance composite materials. He has worked extensively on the impact response of composites and sandwich structures as well as on characterizing the blast response of lightweight structures. He has also worked on developing hybrid materials, such as thermoplastic fiber metal laminates, based on combinations of metal alloys and fiber-reinforced thermoplastic composites. Other areas of research include smart materials, where fiber Bragg grating and plastic optical fibers have been embedded in composites and FMLs, and 3D metal printing, where complex lattice structures have been manufactured and tested under extreme conditions. Wesley Cantwell has published over 220 journal articles and currently serves on the Editorial Board of a number of international journals, including Composites Science and Technology and the International Journal of Impact Engineering. He has also given keynote addresses at many international conferences, including the European Conference on Composite Materials and the International Conference on Composite Science and Technology.

Selected Publications:
Cantwell, W. J. and Morton, J. [1989] “ Comparison of the low and high velocity impact response of CFRP,” Composites 20(6), 545–551.
Cantwell, W. J. and Morton, J. [1990] “ Impact perforation of carbon fibre reinforced,” Composites Science and Technology 38(2), 119–141.
W. J. Cantwell, M. Busser and H. H. Kausch. Computer Engineering, (1991) 1:293307.
W.J. Cantwell, J. Morton, The impact resistance of composite materials - a review, Composites, 22 (5) (1991), pp. 347-362
W. J. Cantwell, C. Dirat and H. H. Kausch, “Comparative Study of the Mechanical Properties of Sandwich Materials for Nautical Construction”, SAMPE J, (1994) 30:45-5 1.
G Reyes, WJ Cantwell, The mechanical properties of fibre-metal laminates based on glass fibre-reinforced polypropylene, Comp Sci Technol, 60 (2000), pp. 1085-1094
Hazizan AM and Cantwell WJ. The low velocity impact response of foam-based sandwich structures. Composites Part B: engineering, 2002; 33: 193–204. 

Hazizan AM and Cantwell WJ. The low velocity impact response of an aluminium honeycomb sandwich structure. Composites Part B: engineering, 2003; 34: 679–687. 

Villanueva GR and Cantwell WJ. Low velocity impact response of novel fiber-reinforced aluminium foam sandwich structures, Journal of Materials Science Letters, 2003; 22: 417–422. 

Kiratisaevee H and Cantwell WJ. The failure behavior of aluminium foam sandwich structures based on fiber reinforced thermoplastics. Journal of Sandwich Structures and Materials, 2003; 5: 53–75
Villanueva GR and Cantwell WJ. The high velocity impact response of composite and FML-reinforced sandwich structures. Composites Science and Technology, 2004; 64: 35–54.
Kiratisaevee H and Cantwell WJ. The impact response of aluminium foam sandwich structures based on a glass fiber-reinforced polypropylene fiber-metal laminate. Polymer Composite, 2004; 25(5): 499–509.


Page 192 / 462