LS-DYNA Implemented Fabric Material Model Development for Engine Fragment Mitigation

This document is a proposal for the development and validation of a constitutive material model for Kevlar and Zylon fabrics to be used with the LS-DYNA Explicit finite element analysis program. Modeling dry fabric behavior when subjected to impact loads is a challenging task for a number of reasons. However, a systematic approach can be used in the development of the material model and the model verified with the large amount of experimental data that is available for these fabrics.

  • Supplemental Notes:
    • Program Information: Aviation Grants


  • English


  • Status: Active
  • Contract Numbers:


  • Sponsor Organizations:

    Federal Aviation Administration

    William J. Hughes Technical Center, Atlantic City International Airport
    Atlantic City, NJ  United States  08405
  • Project Managers:

    Altobelli, Donald

  • Performing Organizations:

    Arizona State University, Tempe

    Tempe, AZ  United States 
  • Start Date: 20060627
  • Expected Completion Date: 0
  • Actual Completion Date: 20120731
  • Source Data: RiP Project 30178

Subject/Index Terms

Filing Info

  • Accession Number: 01478849
  • Record Type: Research project
  • Source Agency: Department of Transportation
  • Contract Numbers: 2006-G-007
  • Files: RiP
  • Created Date: Apr 19 2013 1:01AM