Skip to main content
Log in

Biaxial testing of composite tubes

  • Published:
Experimental Mechanics Aims and scope Submit manuscript

Abstract

The development of a tubular test specimen for the characterization of advanced composite-material lamina and laminate mechanical properties is presented. The specimen design and supporting analyses are given for a practical tubular specimen that minimizes end effects. Test results for simplified loading conditions are shown to be in good agreement with values obtained in other tests. Failure strains in laminates are higher than those obtained in comparable flat-coupon tests. The results obtained indicate that the specimen and apparatus are useful for obtaining response properties and failure values under general in-plane loading.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. Liber, T., Daniel, I.M., LaBedz, R. and Niiro, T., “Fabrication and Testing of Composite Ring Specimens,” Proc. SPI, New Orleans (Feb. 1979).

  2. Whitney, J.M., “Free-Edge Effects in the Characterization of Composite Materials,” Analysis of the Test Methods for High Modulus Fibers and Composites, ASTM STP 521, 167–180 (1973).

    Google Scholar 

  3. Daniel, I.M. et al.Biaxial Testing of Graphite/Epoxy Composites Containing Stress Concentrations,”Final Tech. Rep. AFML-TR-76-244, Air Force Materials Laboratory, Air Force Systems Command, Wright-Patterson AFB, OH (Sept. 1976).

    Google Scholar 

  4. Broutman, L.J. and Krock, R.H., Composite Materials,8,Academic Press (1975).

  5. Guess, T.R. andGerstle, F.P., “Deformation and Fracture of Resin Matrix Composites in Combined Stress States,”J. Comp. Mat.,11,146 (April 1977).

    Google Scholar 

  6. Daniel, I.M., Liber, T., Vanderby, R. and Keller, G.M., “Stress Analysis of Tubular Specimen for Biaxial Testing of Composite Laminates,” Proc. 16th Mtg. Soc. of Eng. Sci., Evanston, IL (Sept. 1979).

  7. Duggen, M.F. and Bailie, J.A., “A New Test Specimen Geometry for Achieving Uniform Biaxial Stress Distributions in Laminated Composite Cylinders,” submitted to 3rd Int. Conf. on Comp. Mat., Paris, France (August 1980).

  8. Wu, E.M. andScheublein, J.K., “Laminate Strength — A Direct Characterization Procedure,” Composite Materials: Testing and Design (3rd Conf.), ASTM STP 546, 188–206 (1974).

    Google Scholar 

  9. Soden, P.D., Leadbetter, P.R., Griggs, P.R. and Eckold, G.C., “The Strength of a Filament Wound Composite Under Biaxial Loading,” Composites, 247 (Oct. 1978).

  10. Halpin, J.C., Pagano, N.J., Whitney, J.M. andWu, E.M., “Characterization of Anisotropic Composite Materials,” Composite Materials: Testing and Design, ASTM STP 460, 37–47 (1969).

    Google Scholar 

  11. Whitney, J.M., Pagano, N.J. andPipes, R.B., “Design and Fabrication of Tubular Specimens for Composite Characterization,” Composite Materials: Testing and Design (2nd conf.), ASTM STP 497, 52–67 (1971).

    Google Scholar 

  12. Pagano, N.J. andWhitney, J.M., “Geometric Design of Composite Cylindrical Characterization Specimens,”J. Comp. Mat.,4,360 (July 1970).

    Google Scholar 

  13. Cook, R.D., Concepts and Applications of Finite Element Analysis, John Wiley and Sons, New York, NY (1974).

    Google Scholar 

  14. Lekhnitskii, S.C., Theory of Elasticity of an Anisotropic Elastic Body, Holden-Day Inc. (1963).

  15. Tsai, S.W. and Hahn, H.T., Introduction to Composite Materials, Technomic Publishing Co. (1980).

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

About this article

Cite this article

Toombes, G.R., Swanson, S.R. & Cairns, D.S. Biaxial testing of composite tubes. Experimental Mechanics 25, 186–192 (1985). https://doi.org/10.1007/BF02328810

Download citation

  • Received:

  • Revised:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF02328810

Keywords

Navigation