1. Hart-Smith LJ. The Ten-Percent Rule for preliminary sizing of fibrous composite structures. McDonnell Douglas Paper MDC 92K0024, SAWE Paper No. 2054, presented to 51st SAWE International Conference, Hartford, Connecticut, 18–20 May, 1992; published in SAWE Journal, Winter 1992, pp. 29–45; also published by Aerospace Materials, Vol. 5, No. 2. August–October 1993. p. 10–16.
2. Hart-Smith LJ. Design and Development of the First Lear Fan All-Composite Aircraft. Douglas Paper 8184, Presented as Keynote address to Institution of Mechanical Engineers Conference on Advanced Composites, London; 7–8 March 1989.
3. Lamina properties and lay-up configurations and loading conditions of a range fibre reinforced composite laminates;Soden;Compos. Sci. Technol.,1998
4. Hart-Smith LJ. Simplified estimation of stiffness and biaxial strengths for design of carbon-epoxy composite structures. Douglas Paper 7548, presented to Seventh Conference on Fibrous Composites in Structural Design, Denver, Colorado, 17–20 June 1985; in Proceedings, AFWAL-TR-85–3094, pp. V(a)-17 to -52. (Subsequently cleared for unlimited distribution.).
5. Hart-Smith LJ. Predictions of a generalized maximum-shear-stress failure criterion for certain fibrous composite laminates, McDonnell Douglas Paper MDC 97K0011, companion paper to the present. Composites Science and Technology 1998; 58(7): 1179–208.