Mechanical Concept of W-WING Whirl Flutter Demonstrator
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F14%3A%230001689" target="_blank" >RIV/00010669:_____/14:#0001689 - isvavai.cz</a>
Alternative codes found
RIV/00010669:_____/15:#0001872
Result on the web
<a href="http://pig.sagepub.com/content/early/2014/10/13/0954410014554473" target="_blank" >http://pig.sagepub.com/content/early/2014/10/13/0954410014554473</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1177/0954410014554473" target="_blank" >10.1177/0954410014554473</a>
Alternative languages
Result language
angličtina
Original language name
Mechanical Concept of W-WING Whirl Flutter Demonstrator
Original language description
This paper deals with the mechanical concept of a whirl flutter aeroelastic demonstrator. It works out the previous study on theW-WING demonstrator design and summarises the new achievements. The paper gives a theoretical background of the subjected whirl flutter phenomenon and summarises the whirl flutter occurrence in aerospace practice. The second part is focused on the experimental research of whirl flutter. At first, a brief summary of past main developments in this field is provided. The main partdeals with the new aeroelastic demonstrator W-WING, designed and developed at the VZLU. The demonstrator represents wing and engine of a twin turboprop commuter aircraft. Contrary to the most of past demonstrators, it includes thrusting propeller. The demonstrator allows changes of the main structural parameters influencing whirl flutter stability characteristics. The demonstrator is intended for experimental investigations at the VZLU 3m-diameter low-speed wind tunnel. The results will
Czech name
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Czech description
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Classification
Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2015
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
ISSN
0954-4100
e-ISSN
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Volume of the periodical
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Issue of the periodical within the volume
published on-line before print
Country of publishing house
GB - UNITED KINGDOM
Number of pages
10
Pages from-to
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UT code for WoS article
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EID of the result in the Scopus database
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