Numerical Simulation of Aircraft over Run Arresting System

Fei Xu; Ze Tan; Ya Jie Shi

doi:10.4028/www.scientific.net/AMR.787.485

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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 787Numerical Simulation of Aircraft over Run...

Numerical Simulation of Aircraft over Run Arresting System

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.

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Periodical:

Advanced Materials Research (Volume 787)

Pages:

485-489

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.787.485

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Online since:

September 2013

Authors:

Fei Xu, Ze Tan, Ya Jie Shi

Keywords:

Aircraft Overrun, EMAS, Foam Concrete, Numerical Simulation

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References

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