Volume 14, Issue 2, 2005

Effect of Thermal Shock on Flexural Modulus of Thermally and Cryogenically Conditioned Kevlar/Epoxy Composites

B. C. RAY

Department of Metallurgical and Materials Engineering, National Institute of Technology, Rourkela- 769008, INDIA

(Received 9/03; accepted 4/04)

Abstract
The utilisation of polymeric matrix composite materials in safety critical structures necessitates their full characterisation especially where changing temperature environment is a concern. An attempt has been made here to assess the effects of thermal shocks on flexural modulus of thermally and cryogenically conditioned Kevlar/epoxy composites. Thermal and cryogenic conditionings were concurrently followed by downthermal shock (positive to negative temperature excursion) and upthermal shock (negative to positive temperature excursion) treatments respectively on the composite laminates. Residual thermal stresses developed by temperature gradient should be given critical attention in many application areas. The 3-point short beam shear (SBS) test was conducted on the conditioned specimens to evaluate modulus. The test results may indicate the relative level of bond strength in a composite system where only the bonding level is a variable. Post-curing strengthening effect of thermal conditioning and mechanical keying factor of cryogenic conditioning are investigated here by scanning electron micrographs. The high radial expansion coefficient of Kevlar fibre causes weakening of interfacial adhesion under the influence of temperature gradient. However, the weak interface may readily allow crack deflection along the interface and improves energy-absorbing capacity.