Experimental analysis of normal and oblique high velocity impacts on carbon/epoxy tape laminates Articles uri icon

publication date

  • May 2014

start page

  • 24

end page

  • 31


  • 60

International Standard Serial Number (ISSN)

  • 1359-835X

Electronic International Standard Serial Number (EISSN)

  • 1878-5840


  • In this work, the effect of high velocity impacts on carbon/epoxy tape quasi-isotropic laminates is studied. Experimental test were carried out at two different impact angles and in a wide range of velocities (from 80 to 490 m/s). Both parameters, the residual velocity and the damaged area, are used to evaluate the effect of the kinetic energy of the projectile on the laminate response. In addition it has been proposed a simplified analytical model which allows to identify the different energy absorbtion mechanisms and predict the residual velocity of the projectile. Finally the energy absorbed by the laminate during the impact is studied.


  • Mechanical Engineering


  • d. obliquity; d. high velocity impact; a. tape laminate; a. carbon/epoxy