Detail publikace

Dynamic tests of composite panels of an aircraft wing

ŠPLÍCHAL, J. PÍŠTĚK, A. HLINKA, J.

Originální název

Dynamic tests of composite panels of an aircraft wing

Typ

článek v časopise ve Web of Science, Jimp

Jazyk

angličtina

Originální abstrakt

The paper describes the analysis of aerospace composite structures under dynamic loading. Today, it is common to use design procedures based on assumption of static loading only, and dynamic loading is rarely assumed and applied in design and certification of aerospace structures. The paper describes the application of dynamic loading for the design of aircraft structures, and the validation of the procedure on a selected structure. The goal is to verify the possibility of reducing the weight through improved design/modelling processes using dynamic loading instead of static loading. The research activity focuses on the modelling and testing of a composite panel representing a local segment of an aircraft wing section, investigating in particular the buckling behavior under dynamic loading. Finite Elements simulation tools are discussed, as well as the advantages of using a digital optical measurement system for the evaluation of the tests. The comparison of the finite element simulations with the results of the tests is presented.

Klíčová slova

Stiffened panel , Buckling , Finite element method , Testing

Autoři

ŠPLÍCHAL, J.; PÍŠTĚK, A.; HLINKA, J.

Rok RIV

2015

Vydáno

1. 10. 2015

Nakladatel

PERGAMON-ELSEVIER SCIENCE LTD

Místo

THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, ENGLAND

ISSN

0376-0421

Periodikum

PROGRESS IN AEROSPACE SCIENCES

Ročník

2015

Číslo

78

Stát

Spojené státy americké

Strany od

50

Strany do

61

Strany počet

12

URL

BibTex

@article{BUT114836,
  author="Jan {Šplíchal} and Antonín {Píštěk} and Jiří {Hlinka}",
  title="Dynamic tests of composite panels of an aircraft wing",
  journal="PROGRESS IN AEROSPACE SCIENCES",
  year="2015",
  volume="2015",
  number="78",
  pages="50--61",
  doi="10.1016/j.paerosci.2015.05.005",
  issn="0376-0421",
  url="http://www.sciencedirect.com/science/article/pii/S0376042115000366"
}