Landing Shock Aeroelastic Response Analysis of EV 55M Utility Aircraft

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F12%3A%230001555" target="_blank" >RIV/00010669:_____/12:#0001555 - isvavai.cz</a>

Result on the web

<a href="http://www.czaerospace.eu/en/2012-03-45.html" target="_blank" >http://www.czaerospace.eu/en/2012-03-45.html</a>

DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Landing Shock Aeroelastic Response Analysis of EV 55M Utility Aircraft

Original language description

The paper deals with the EV-55M aircraft landing shock aeroelastic response analysis. The analysis was performed as a part of the aircraft certification in order to fulfill the CS / FAR 23 § 23.479(d) regulation requirement. The FE model used for the former flutter analyses was utilized. The excitation force was based on the landing gear drop test results. The airflow parameters were set according the aircraft flight envelope and the regulation statements. The modal transient aeroelastic response solution was employed. The structure response was evaluated at the engine center of gravity and the selected points on the wing

Czech name

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Czech description

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Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

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Continuities

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2012

Confidentiality

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

Name of the periodical

Czech Aerospace Proceedings / Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Volume of the periodical

3/2012

Issue of the periodical within the volume

3

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

2

Pages from-to

1-2

UT code for WoS article

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EID of the result in the Scopus database

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