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JEBÁČEK, I.
Originální název
FUSELAGE TEST OF A SMALL AIRCRAFT ACCORDING CS-23 REQUIREMENTS
Typ
článek v časopise - ostatní, Jost
Jazyk
angličtina
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
Test, Fuselage, Measurement, Force
Autoři
Rok RIV
2009
Vydáno
16. 3. 2009
Nakladatel
Vilnius Gediminas Technical University
Místo
Vilnius
ISSN
1822-4180
Periodikum
AVIATION Research Journal of Vilnius Gediminas Technical University
Ročník
Číslo
13
Stát
Litevská republika
Strany od
26
Strany do
33
Strany počet
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" }