Wind tunnel test of W-WING aeroelastic demonstrator

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F22%3AN0000044" target="_blank" >RIV/00010669:_____/22:N0000044 - 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

Wind tunnel test of W-WING aeroelastic demonstrator

Original language description

This paper discusses the accomplishments in the testing of the W WING whirl flutter demonstrator. First, the paper outlines the theoretical background on the whirl flutter phenomenon and information about the demonstrator itself, past design and development activities and preparatory experiments. The main focus is on the wind tunnel measurements. First and second experimental campaigns are described. The wind tunnel test description includes the test equipment and methodology as well as the test result assessment methodology and examples of the results. Finally, the outcome and future activities are outlined.

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

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OECD FORD branch

20304 - Aerospace engineering

Project

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Continuities

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2022

Confidentiality

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

Article name in the collection

Engineerings Mechanics 2022, Book of Full Texts

ISBN

978-80-86246-48-2

ISSN

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e-ISSN

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Number of pages

4

Pages from-to

57-60

Publisher name

UTAM AV ČR

Place of publication

ČR

Event location

Milovy

Event date

Jan 1, 2022

Type of event by nationality

EUR - Evropská akce

UT code for WoS article

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