1. Hart-Smith, L. J., Approximate analysis methods for fibrous composite laminates under combined biaxial and shear loading. Douglas Aircraft Company, IRAD Report MDC-J9898, March 1984.
2. Hart-Smith, L. J. Predicting the strength of fibrous composites by an orthotropic generalization of the maximum-shear-stress (Tresca) condition, McDonnell Douglas Paper MDC 91K0068. Presented to Second SERC-I.Mech.E. Expert Meeting, Failure Mechanism(s) and Criteria for Predicting the Performance of Polymer-Based Composite Structures, St. Albans, UK, 23–25 September 1991; published in Proc. Inst’n. Mech. Eng’rs, Part G, Journal of Aerospace Engineering, 1994, 208, 9–18.
3. Hart-Smith, L. J., How to calculate the in-plane strengths of fibre–polymer composites, McDonnell Douglas Paper MDC 92K0023. Presented to 25th MIL-HDBK-17 Meeting, Laughlin, Nevada, 31 March–2 April 1992; published in SAMPE Journal, 1992, 28(6), 25–35.
4. Soden, P. D., Hinton M. J. and Kaddour A. S., Lamina properties, lay-up configurations and loading conditions for a wide range of fibre reinforced composite laminates. Compos. Sci. Technol., 1998, 58(7), 1011.
5. Baker, A. A., Bonded composite repair of metallic aircraft components—overview of Australian activities. AGARD-CP-550, pp. 1.1–1.14.