Detail publikace

SIMULATION OF PILOT LOAD DURING EMERGENCY LANDING CONDITIONS

MALIŠ, M. ŠPLÍCHAL, J.

Originální název

SIMULATION OF PILOT LOAD DURING EMERGENCY LANDING CONDITIONS

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

Models of dummy embedded in numerical commercial software packages are calibrated using Anthropometric Testing Dummies (ATD). The dummies vary according to the loading character different for aeronautic or automotive industries. The aim of the article is to find a solution of analysis of loads in lumbar column, based on aeronautical regulation requirements using available dummies in commercial software systems MSC.Nastran and MSC.Dytran. Simulation results were compared with experimental test data obtained from dynamic sled test with implemented ATD

Klíčová slova

Aircraft passive safety, Finite element method, Dummy, Dynamic test

Autoři

MALIŠ, M.; ŠPLÍCHAL, J.

Vydáno

15. 5. 2017

Nakladatel

Brno University of Technology

Místo

konference Engineering Mechanics 2017, Svratka, ČR

ISBN

978-80-214-5497-2

Kniha

Engineering Mechanics 2017

Edice

1

ISSN

1805-8248

Periodikum

Engineering Mechanics ....

Stát

Česká republika

Strany od

610

Strany do

613

Strany počet

4

URL

http://www.engmech.cz/im/doc/EM2017_proceedings_all.pdf

BibTex

@inproceedings{BUT140212,
  author="Michal {Mališ} and Jan {Šplíchal}",
  title="SIMULATION OF PILOT LOAD DURING EMERGENCY LANDING CONDITIONS",
  booktitle="Engineering Mechanics 2017",
  year="2017",
  series="1",
  journal="Engineering Mechanics ....",
  pages="610--613",
  publisher="Brno University of Technology",
  address="konference Engineering Mechanics 2017, Svratka, ČR",
  isbn="978-80-214-5497-2",
  issn="1805-8248",
  url="http://www.engmech.cz/im/doc/EM2017_proceedings_all.pdf"
}