Aeroelastic Sensitivity Analysis of Airliner Wing

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F14%3A%230001874" target="_blank" >RIV/00010669:_____/14:#0001874 - isvavai.cz</a>

Result on the web

<a href="http://www.engineeringmechanics.cz/obsahy.html?R=21&C=1" target="_blank" >http://www.engineeringmechanics.cz/obsahy.html?R=21&C=1</a>

DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Aeroelastic Sensitivity Analysis of Airliner Wing

Original language description

This paper describes the airliner wing flutter sensitivity analysis. The sensitivity coefficients define the influence of the structural parameter changes on the structure eigenvalue and flutter stability characteristics. Evaluated structural parametersrepresent the possible changes of the structure due to the installation of the smart high-lift devices at the leading and trailing edge region. The main aim of the presented work is to evaluate the impact of components to the stability and to define themost critical regions or parameters.

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

2014

Confidentiality

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

Name of the periodical

Engineering Mechanics

ISSN

1210-2717

e-ISSN

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Volume of the periodical

21

Issue of the periodical within the volume

1

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

8

Pages from-to

3-10

UT code for WoS article

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EID of the result in the Scopus database

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