Publication detail

FUSELAGE TEST OF A SMALL AIRCRAFT ACCORDING CS-23 REQUIREMENTS

JEBÁČEK, I.

Original Title

FUSELAGE TEST OF A SMALL AIRCRAFT ACCORDING CS-23 REQUIREMENTS

Type

journal article - other

Language

English

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

Test, Fuselage, Measurement, Force

Authors

JEBÁČEK, I.

RIV year

2009

Released

16. 3. 2009

Publisher

Vilnius Gediminas Technical University

Location

Vilnius

ISBN

1822-4180

Periodical

AVIATION Research Journal of Vilnius Gediminas Technical University

Year of study

2009

Number

13

State

Republic of Lithuania

Pages from

26

Pages to

33

Pages count

8

BibTex

@article{BUT48971,
  author="Ivo {Jebáček}",
  title="FUSELAGE TEST OF A SMALL AIRCRAFT ACCORDING CS-23 REQUIREMENTS",
  journal="AVIATION 
Research Journal of Vilnius Gediminas Technical University",
  year="2009",
  volume="2009",
  number="13",
  pages="26--33",
  issn="1822-4180"
}