Detail publikace

3D Fabric Application on Glider Structures

JURAČKA, J.

Originální název

3D Fabric Application on Glider Structures

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

A material, called the Paraglass, has been used for the design of the ultralight composite glider, as a substitute for foam at sandwich structure. The material is used as middle lay of all coverings, which are the skin of wing, the fuselage and the tailplane. The advantage of this material is very simple and cheap technology of the structure production. The disadvantage is its weight and density. Before putting into production of aircraft, basic material tests were done to determinate tensile strength and shear behaviour. The test results confirmed behaviour like isotropic panel. On the basis of results of initial tests and analyses, the lamination of the wing skin and fuselage was designed. Both wing and fuselage were tested and they provided the ability to carry ultimate loads.

Klíčová slova

parabeam, paraglass, form, 3D, share test, composite material

Autoři

JURAČKA, J.

Rok RIV

2005

Vydáno

13. 3. 2005

Nakladatel

The Royal Aeronautical Society, Australia

Místo

Melbourne, Austálie

ISBN

0-85825-732-7

Kniha

CD-Rom of Congress proceedings

Strany od

1

Strany do

100

Strany počet

100

BibTex

@inproceedings{BUT16865,
  author="Jaroslav {Juračka}",
  title="3D Fabric Application on Glider Structures",
  booktitle="CD-Rom of Congress proceedings",
  year="2005",
  pages="100",
  publisher="The Royal Aeronautical Society, Australia",
  address="Melbourne, Austálie",
  isbn="0-85825-732-7"
}