Numerical simulation of aircraft over run arresting system

Fei Xu, Ze Tan, Ya Jie Shi

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Scopus citations

Abstract

Engineered Material Arresting System (EMAS) is the specified equipment used to prevent aircraft from overrunning. Based on static compression and impact tests of the foam concrete, material model and parameters in the FEM simulation are determined. Then numerical simulations are performed on FAA(Federal Aviation Administration) aircraft arresting tests. The simplified aircraft arresting FEM model and corresponding simulation method are verified. The thickness effect of the arresting bed is studied.

Original languageEnglish
Title of host publicationAdvanced Materials Researches, Engineering and Manufacturing Technologies in Industry
Pages485-489
Number of pages5
DOIs
StatePublished - 2013
Event2013 2nd International Symposium on Materials Science and Engineering Technology, ISMSET 2013 - Guangzhou, China
Duration: 27 Jun 201328 Jun 2013

Publication series

NameAdvanced Materials Research
Volume787
ISSN (Print)1022-6680

Conference

Conference2013 2nd International Symposium on Materials Science and Engineering Technology, ISMSET 2013
Country/TerritoryChina
CityGuangzhou
Period27/06/1328/06/13

Keywords

  • Aircraft overrun
  • EMAS
  • Foam concrete
  • Numerical simulation

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