Flutter Analysis of Twin Turboprop Aircraft with Tip-tanks

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F18%3AN0000010" target="_blank" >RIV/00010669:_____/18:N0000010 - isvavai.cz</a>
Result on the web
<a href="http://www.icas.org/ICAS_ARCHIVE/ICAS2018/data/papers/ICAS2018_0004_paper.pdf" target="_blank" >http://www.icas.org/ICAS_ARCHIVE/ICAS2018/data/papers/ICAS2018_0004_paper.pdf</a>
DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Flutter Analysis of Twin Turboprop Aircraft with Tip-tanks
Original language description
This paper deals with aeroelastic (flutter) analysis of an aircraft with unconventional wing structure, which is specific by the installation of wing-tip tanks. In addition, the wing configuration without tip-tanks is also applicable at aircraft operation. The subjected aircraft is twin wing-mounted tractor turboprop commuter aircraft for 19 passengers, with a wingspan of 9.6 m and a maximal take-off weight of 7000 kg. The paper is focused on the assessment of specific flutter issue, originating from the unconventional wing configuration. Further, another specific flutter issues related to elevator flutter and rudder flutter are described.
Czech name
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Czech description
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Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2018
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018
ISBN
978-3-932182-88-4
ISSN
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e-ISSN
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Number of pages
7
Pages from-to
nestránkováno
Publisher name
International council of the aeronautical sciences
Place of publication
Amsterdam
Event location
Belo Horizonte, Brasil
Event date
Sep 9, 2018
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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