Publication detail

Ruckling and Failure of Composite Web

JURAČKA, J.

English title

Ruckling and Failure of Composite Web

Type

Paper in proceedings (conference paper)

Language

en

Original abstract

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.

Keywords in English

Composite Web

Released

2002-12-01

Publisher

VGTU

Location

Vilnius, Lithuania

ISBN

9986-05-571-7

Book

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

Pages from–to

54–

Pages count

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"
}