Detail publikace

Comparison of Hard and Soft Soil Impact Surface in Glider Crashworthiness Test Simulation

MALIŠ, M.

Anglický název

Comparison of Hard and Soft Soil Impact Surface in Glider Crashworthiness Test Simulation

Typ

Článek recenzovaný mimo WoS a Scopus

Jazyk

en

Originální abstrakt

Abstract. The article describes compliance evaluation of a glider cockpit crashworthiness numerical simulation using a static test. The design of the test and the numerical simulation model were prepared in accordance with the CS 22.561(b)(2) requirements. The next part demonstrates a comparison of two crash test simulations to the hard and soft soil impact surface. Injury criteria were used to evaluate the simulations. The whole simulation was developed using nonlinear explicit transient dynamic computer code MSC. Dytran. Both the test and the simulations were carried out by the Institute of Aerospace Engineering, Brno University of Technology.

Klíčová slova anglicky

Crashworthiness, Glider, Soft Soil surface, Hard surface, finite elemnt method, simulation

Vydáno

2008-10-15

Nakladatel

Czech Aerospace manufacturers Association

Místo

Praha

ISSN

1211-877X

Časopis

Letecký zpravodaj

Ročník

2008

Číslo

2

Strany od–do

20–25

Počet stran

64

BIBTEX


@article{BUT49164,
  author="Michal {Mališ}",
  title="Comparison of Hard and Soft Soil Impact Surface in Glider Crashworthiness Test Simulation",
  journal="Letecký zpravodaj",
  year="2008",
  volume="2008",
  number="2",
  pages="20--25",
  issn="1211-877X"
}