Detail publikace

Ruckling and Failure of Composite Web

JURAČKA, J.

Originální název

Ruckling and Failure of Composite Web

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

Laboratory of aircraft technology of the Institute of Aerospace Engineering has been gradually gained some experience in the field of testing and behaviour of the composite aircraft wing structures. The latest test was the wing of the successful ultralight aircraft TL-2000 Carbon Sting. The tests and measurements, done with this wing, should have helped to evaluate and compare the root part of the wing structure, i.e. the root part of the beam in front of and behind the root rib, the typical web parts of the root rib and the parts of root web under the point of application of local force.

Klíčová slova

Composite Web

Autoři

JURAČKA, J.

Rok RIV

2002

Vydáno

1. 12. 2002

Nakladatel

VGTU

Místo

Vilnius, Lithuania

ISBN

9986-05-571-7

Kniha

Fifth International Seminar on RECENT RESEARCH AND DESIGN PROGRESS IN AERONAUTICAL ENGINEERING AND INFLUENCE ON EDUCATION, Book of Abstracts

Edice

NEUVEDENO

Číslo edice

NEUVEDENO

Strany od

54

Strany do

54

Strany počet

1

BibTex

@inproceedings{BUT10543,
  author="Jaroslav {Juračka}",
  title="Ruckling and Failure of Composite Web",
  booktitle="Fifth International Seminar on RECENT RESEARCH AND DESIGN PROGRESS IN AERONAUTICAL ENGINEERING AND INFLUENCE ON EDUCATION, Book of Abstracts",
  year="2002",
  pages="1",
  publisher="VGTU",
  address="Vilnius, Lithuania",
  isbn="9986-05-571-7"
}