Murray L. Scott
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- Computer modelling of impact on curved fibre composite panels. Dans: Composite Structures, v. 47, n. 1-4 (décembre 1999). (1999):
- Experience with the finite element modelling of a full-scale test of a composite aircraft control surface. Dans: Composite Structures, v. 50, n. 4 (décembre 2000). (2000):
- Parametric optimisation of composite shell structures for an aircraft Krueger flap. Dans: Composite Structures, v. 57, n. 1-4 (juillet 2002). (2002):
- The analysis of skin-to-stiffener debonding in composite aerospace structures. Dans: Composite Structures, v. 57, n. 1-4 (juillet 2002). (2002):
- The case for multidisciplinary design approaches for smart fibre composite structures. Dans: Composite Structures, v. 58, n. 3 (novembre 2002). (2002):
- Influence of post-buckling behaviour of composite stiffened panels on the damage criticality. Dans: Composite Structures, v. 66, n. 1-4 (octobre 2004). (2004):
- Review of delamination predictive methods for low speed impact of composite laminates. Dans: Composite Structures, v. 66, n. 1-4 (octobre 2004). (2004):
- Thickness effects on the compressive stiffness and strength of stitched composite laminates. Dans: Composite Structures, v. 66, n. 1-4 (octobre 2004). (2004):