FEM Model of Airframe Fuselage Part

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F07%3A00424156" target="_blank" >RIV/60162694:G43__/07:00424156 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

FEM Model of Airframe Fuselage Part

Original language description

The paper deals with the proposal of FEM model of a helicopter fuselage part using SW Ansys. FEM model is a semimonocoque structure consisting of spars, ribs and skin. The model follows practical experiments on real structure loaded by bending and torsion moments. The load is based upon a limit airplane load. Proposal model helps to simulate the battle damages and to predict their effect on operational and flight helicopter capabilities. Some operational damages were carried out on the model and experimental part as well. The simulation is compared to practical experiments and influencing factors are disscussed.

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

KA - Militarism

OECD FORD branch

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Project

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Continuities

S - Specificky vyzkum na vysokych skolach

Publication year

2007

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection

Konference ICMT 2007

ISBN

978-80-7231-238-2

ISSN

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e-ISSN

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Number of pages

6

Pages from-to

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Publisher name

Univerzita obrany Brno

Place of publication

Brno

Event location

Brno

Event date

Jan 1, 2007

Type of event by nationality

EUR - Evropská akce

UT code for WoS article

000263292800045