Publication detail

SIMULATION OF PILOT LOAD DURING EMERGENCY LANDING CONDITIONS

MALIŠ, M. ŠPLÍCHAL, J.

Original Title

SIMULATION OF PILOT LOAD DURING EMERGENCY LANDING CONDITIONS

Type

conference paper

Language

English

Original Abstract

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

Keywords

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

Authors

MALIŠ, M.; ŠPLÍCHAL, J.

Released

15. 5. 2017

Publisher

Brno University of Technology

Location

konference Engineering Mechanics 2017, Svratka, ČR

ISBN

978-80-214-5497-2

Book

Engineering Mechanics 2017

Edition

1

ISBN

1805-8248

Periodical

Engineering Mechanics ....

State

Czech Republic

Pages from

610

Pages to

613

Pages count

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"
}