Carbon-carbon coupons were loaded and unloaded in uniaxial tension to progressively higher loads. Hysteresis in the material was noted especially after the stress-strain curves became nonlinear at about 2000 μ. Each subsequent reloading showed an increase in the linear range similar to work hardening in metals except that the modulus was lower on each cycle. The onset of acoustic emission was monitored on each cycle and the computed felicity ratio correlated with the change in stiffness.
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References
1.
1. Beuchler, M., G. M. Hawkins and R. A. Meyer. 1985 Astronautics Laboratory Contractor Report, AFRPL TR-85–062, Air Force Systems Command, Edwards AFB, CA 93923–5000.
2.
2. Dvorak, G. J., N. Laws and M. Hejazi. 1985. Journal of Composite Materials, 19: 216.
3.
3. Reifsnider, K. L., E. G. Henneke, W. W. Stinchcomb and J. C. Duke. 1983. In Mechanics of Composite Materials/Recent Advances, Z. Hashin and C. T. Herakovich, eds., Pergamon Press.
4.
4. Fowler, T. J.1977. “Preprint 3092,” paper presented at The ASCE Fall Convention, San Francisco, CA, Oct. 17–21, 1977; New York: American Society of Civil Engineers.
5.
5. Gorman, M. R. and T. H. Rytting. 1983. Proceedings of the First ICARP, San Francisco, CA.
6.
6. Awerbuch, J. and S. Ghaffari. 1986. Proceedings of the Second ICARP, Montreal, Canada.
7.
7. Kachanov, L. M.1986. Introduction to Continuum Damage Mechanics.Martinus Nijhoff Publishers.