## Chapter 9: References

1. S. Hiermaier, W. Riedel, C.J. Hayhurst, R.A. Clegg, C.M. Wentzel, Advanced Material Models for Hypervelocity Impact Simulations, EMI-Report No. E43/99, ESA CR(P) 4305, 1999.

2. W. Riedel, W. Harwick, D.M. White, R.A. Clegg, Advanced Material Damage Models for Numerical Simulation Codes, EMI-Report No. I 75/03, ESA CR(P) 4397, October 2003.

3. J.K. Chen, F.A.Allahdadi, C.T.Sun, “A Quadratic Yield Function for Fiber-Reinforced Composites“, Journal of Composite Materials, vol. 31, No. 8, 1997.

4. C.T. Sun and S. Li, “Three-Dimensional Effective Elastic Constants for Thick Laminates”, Journal of Composite Materials, vol. 22, 1988.

5. C.E. Anderson, P.A. Cox, et. al. “A Constitutive Formulation for Anisotropic Materials Suitable for Wave Propagation Computer programme-II”, Comp. Mech., vol. 15, p201-223, 1994.

6. J.P. Hou, N. Petrinic, C. Ruiz, “Prediction of Impact Damage in Composite Plates”, Comp. In Sc. and Tech., 60, 273-281, 2000.

7. R.M. Jones, “Mechanics of Composite Materials”, McGraw-Hill, 1975.

8. M.A. Meyers, “Dynamic Behavior of Materials”, John Wiley & Sons, 1994 – ISBN 0-471-58262-X.

9. W.C. Kim, C.K.H. Dharan, Analysis of five-point bending for determination of the interlaminar shear strength of unidirectional composite materials, Composite Structures, Vol. 30, 1995, 241-251.

10. ASTM standard D3846-79 (1985), ASTM Standards and Literature References for Composite Materials, 2nd Ed., American Society for Testing and Materials, Philadelphia, PA, 1990.

11. Luft- und Raumfahrt, Kohlenstoffaserverstärkte Kunstoffe, Prüfverfahren, Bestimmung der interlaminaren Energiefreisetzungsrate, Mode II,G/IIC, DIN EN 6034, April 1996.

12. C.J. Hayhurst, J.G. Leahy, M. Deutekom, M. Jacobs, P. Kelly, “Development of Material Models for Numerical Simulation of Ballistic Impact onto Polyethylene Fibrous Armour”, presented at PASS, Colchester, UK, 2000.

13. R.A. Clegg, C.J. Hayhurst, J.G. Leahy, M. Deutekom,. “Application of a Coupled Anisotropic Material Model to High Velocity Impact of Composite Textile Armour”, presented at the 18th Int. Symposium on Ballistics, San Antonio, USA, 1999

14. D.M. White, E.A. Taylor, R.A. Clegg, “Numerical Simulation and Experimental Characterisation of Direct Hypervelocity Impact on a Spacecraft Hybrid Carbon Fiber/Kevlar Composite Structure”, Int. J. Impact Eng., vol. 29, 2003, pp779-790.

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