Publication detail

FUSELAGE TEST OF A SMALL AIRCRAFT ACCORDING CS-23 REQUIREMENTS

JEBÁČEK, I.

English title

FUSELAGE TEST OF A SMALL AIRCRAFT ACCORDING CS-23 REQUIREMENTS

Type

Peer-reviewed article not indexed in WoS or Scopus

Language

en

Original abstract

This article describes a static strength test of a fuselage of a small aircraft. Tests were done according CS-23 requirements. The test program was analyzed firstly and then was created a methodology of a whole test and the test could be built. The submitter requirement was that the bending and torque moment and shear force have to be as close as possible to calculated loads. This problem takes out a many loading forces along the fuselage length and we had to solve how to load a several tons along the seven meters. For this purpose the loading tree and rollers were used. The result of this article says, what the forces are changed with using the rollers with combination of loading tree and describes the test arrangement.

Keywords in English

Test, Fuselage, Measurement, Force

Released

2009-03-16

Publisher

Vilnius Gediminas Technical University

Location

Vilnius

ISSN

1822-4180

Journal

Aviation

Volume

2009

Number

13

Pages from–to

26–33

Pages count

8

BIBTEX


@article{BUT48971,
  author="Ivo {Jebáček}",
  title="FUSELAGE TEST OF A SMALL AIRCRAFT ACCORDING CS-23 REQUIREMENTS",
  journal="Aviation",
  year="2009",
  volume="2009",
  number="13",
  pages="26--33",
  issn="1648-7788"
}