journal article·1998-11

Comparison of in situ damage assessment in unbalanced fabric composite and model laminate of planar (one-directional) crimping

A.K. Roy

Composites Science and Technology· Volume 58· Issue 11
Publisher page

Abstract

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Research context

OpenAlex topics: Mechanical Behavior of Composites · Textile materials and evaluations · Structural Analysis and Optimization

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References (12)

Show source-provided references
1. A numerical micromechanics analysis of the mechanical properties of a plain weave composite10.1016/0045-7949(90)90154-T ↗
2. Prediction of on-axes elastic properties of plain weave fabric composites10.1016/0266-3538(92)90036-3 ↗
3. A micromechanics model for thermoelastic properties of plain weave fabric composites10.1115/1.2904322 ↗
4. Modeling weave and stacking configuration effects on interlaminar shear stresses in fabric laminates10.1016/0010-4361(93)90128-U ↗
5. Marrey, R. V. and Sankar, B. V., Micromechanical models for textile structural composites. NASA CR 198229, 1995.
6. Chou, T. and Ko, F. K., Textile Structural Composites, Ch. 7. Elsevier, New York, USA.
7. Failure behavior of plain weave fabric laminates under in-plane shear loading10.1520/CTR10390J ↗
8. Deformation and failure behavior of woven composite laminates10.1115/1.2904277 ↗
9. Whitcomb, J. D., Three-dimensional stress analysis of plain weave composites. In Composite Materials: Fatigue and Fracture, Vol. 3, ed. T. K. O’Brien. ASTM STP 1110, American Society for Testing and Materials, Philadelphia, PA, pp. 417–438.10.1520/STP17730S ↗
10. Roy, A. K., Experimental observation of damage in 8HS fabric composites in tensile loading. Proceedings of the 9th Technical Conference, ed. T.-W. Chou and J. R. Vinson. American Society for Composites, University of Delaware, Newark. Technomic, Lancaster, PA, pp. 1273–1280.
11. In situ damage observation and failure in model laminates containing planar yarn crimping of woven composites10.1002/(SICI)1234-986X(199606)3:2<101::AID-MCM35>3.3.CO;2-2 ↗
12. Stress singularity due to kink band weakening a unidirectional composite under compression10.1177/002199839603000603 ↗