journal article·1995-01

Measurement of thermal strains during compressive fragmentation in single-fibre composites by Raman spectroscopy

Jonathan R. Wood, Yanling Huang, Robert J. Young, Gad Marom

Composites Science and Technology· Volume 55· Issue 3
Publisher page

Abstract

No abstract is available for this record. The assistant can identify its topic from the title, but cannot infer the study’s results.

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Research context

OpenAlex topics: Fiber-reinforced polymer composites · Mechanical Behavior of Composites · Graphene research and applications

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References (16)

Show source-provided references
1. Wood, J. R., Wagner, H. D. & Marom, G., The compressive fragmentation phenomenon: Using microcomposites to evaluate thermal stresses, single fibre compressive strengths, Weibull parameters and interfacial shear strengths. Proc. Roy. Soc. Lond. (in press).10.1098/rspa.1996.0014 ↗
2. The significance of microcomposites as experimental models10.1002/pc.750120404 ↗
3. A model for compressive fragmentation
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5. Analysis of the fragmentation test for carbon fibre/epoxy model composites using Raman spectroscopy10.1016/0266-3538(94)90033-7 ↗
6. Analysis of composite test methods using Raman spectroscopy
7. Interfacial behaviour in a high temperature cured carbon fibre/epoxy resin model composite10.1016/0010-4361(95)92619-N ↗
8. Hull · 1981 · 36
9. Clarifying the application of Weibull statistics for determining the stress state of a fibre from fragmentation tests
10. Axxis · 1993
11. Surface treatment and interlayers for pitch based carbon fibres
12. Huang, Y. & Young, R. J., Effect of fibre microstructure upon the modulus of pan- and pitch-based carbon fibres. Carbon (submitted).10.1016/0008-6223(94)00109-D ↗
13. Interfacial studies on carbon/thermoplastic model composites using laser Raman spectroscopy10.1007/BF00542931 ↗
14. Compressional behaviour of carbon fibres: Part II. Modulus softening10.1007/BF00445995 ↗
15. Hull · 1981 · 24
16. Tensile properties of fibre-reinforced metals: copper/tungsten and copper/molybdenum10.1016/0022-5096(65)90035-9 ↗