Airframe Fuselage FEM Model with Operational Damage

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F07%3A00424158" target="_blank" >RIV/60162694:G43__/07:00424158 - 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

Airframe Fuselage FEM Model with Operational Damage

Original language description

The paper deals with the proposal of FEM model of a helicopter fuselage part using SW Ansys for the operational damage simulation. FEM model is a semimonocoque duraluminium structure using spars, ribs and skin. The model is compared to practical experiments on real structure loaded by bending and torsion moments. The load is based on a limit aircraft load. Simulation influencing factors are discussed.

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 Aeronautika 07

ISBN

978-80-8073-882-2

ISSN

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e-ISSN

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Number of pages

2

Pages from-to

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Publisher name

Technická univerzita Košice

Place of publication

Košice

Event location

Košice

Event date

Jan 1, 2007

Type of event by nationality

EUR - Evropská akce

UT code for WoS article

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