Detail publikace

FUSELAGE TEST OF A SMALL AIRCRAFT ACCORDING CS-23 REQUIREMENTS

JEBÁČEK, I.

Anglický název

FUSELAGE TEST OF A SMALL AIRCRAFT ACCORDING CS-23 REQUIREMENTS

Typ

Článek recenzovaný mimo WoS a Scopus

Jazyk

en

Originální abstrakt

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.

Klíčová slova anglicky

Test, Fuselage, Measurement, Force

Vydáno

2009-03-16

Nakladatel

Vilnius Gediminas Technical University

Místo

Vilnius

ISSN

1822-4180

Časopis

Aviation

Ročník

2009

Číslo

13

Strany od–do

26–33

Počet stran

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"
}