Predictions of a generalized maximum-shear-stress failure criterion for certain fibrous composite laminates

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), 1011.10.1016/S0266-3538(98)00078-5 ↗

5. Baker, A. A., Bonded composite repair of metallic aircraft components—overview of Australian activities. AGARD-CP-550, pp. 1.1–1.14.

6. Puck, A., Festigkeitsberechnung an Glassfaser/Kunstoff-Laminaten bei zusammengesetzter Beanspruchung. Kunststoffe, 1969, 59, 780–787. (English summary: calculating the strength of glassfibre/plastics laminates under combined load. German Plastics, 1969, 59, 18–19.)

7. Hart-Smith, L. J., Predictions of the original and truncated maximum-strain failure models for certain fibrous composite laminates, McDonnell Douglas Paper MDC 97K0010. Compos. Sci. Technol., 1998, 58(7), 1151.10.1016/S0266-3538(97)00192-9 ↗

8. Chamis, C. C., Micromechanics strength theories in Composite Materials, Vol. 5, Fracture and Fatigue, ed. L. J. Broughtman, Academic Press, New York, 1974, pp. 126–131.

9. Jones, R. M., Mechanics of Composite Materials. Scripta, Washington, DC, 1975.10.1115/1.3423688 ↗

10. The mechanics of plastics reinforcement in tension

11. Simplified stress analysis of filament reinforced plastic pressure vessels

12. Black, J. B., Jr and Hart-Smith, L. J., The douglas bonded tapered rail-shear test specimen for fibrous composite laminates, Douglas Paper 7764. In Proceedings of the 32nd International SAMPE Symposium and Exhibition, Anaheim, California, 6–9 April, 1987, pp. 360–372.

13. Hart-Smith, L. J. Generation of higher composite material allowables using improved test coupons. Douglas Paper 8557, in Proceedings of the 36th International SAMPE Symposium and Exhibition, San Diego, California, 15–18 April 1991, pp. 1029–1044; modified and republished in Aerospace Composites & Materials 1991, 3(3), 26–30, 58, and 1991 3(4), 13–16, 18.

14. Hart-Smith, L. J., Backing out equivalent unidirectional lamina strengths from tests on cross-plied laminates, McDonnell Douglas Paper MDC 91K0078. In Proceedings of the 37th International SAMPE Symposium and Exhibition, Anaheim, California, 9–12 March 1992, pp. 977–990.

15. Hart-Smith, L. J., Fibrous composite failure criteria—fact and fantasy, McDonnell Douglas Paper MDC 93K 0047. Presented to Plenary Session of Seventh International Conference on Composite Structures, Paisley, Scotland, 5–7 July 1993; abridgement to be published, under the title: A bona-fide fibrous composite failure criterion in Composites.

16. Hart-Smith, L. J., A re-examination of the analysis of in-plane matrix failures in fibrous composite laminates, McDonnell Douglas Paper MDC 95K0069. Composites Science and Technology 1996, 56(2), 107–121.10.1016/0266-3538(95)00124-7 ↗

17. Rosen, B. W., Fibre composite analysis and design, Material Sciences Corporation, Report DOT/FAA/CT88/18, 1988.