Aeroelastic Analysis of Twin Turboprop Utility Aircraft
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F11%3A%230001140" target="_blank" >RIV/00010669:_____/11:#0001140 - isvavai.cz</a>
Result on the web
<a href="http://pig.sagepub.com/content/225/5.toc" target="_blank" >http://pig.sagepub.com/content/225/5.toc</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1177/09544100JAERO815" target="_blank" >10.1177/09544100JAERO815</a>
Alternative languages
Result language
angličtina
Original language name
Aeroelastic Analysis of Twin Turboprop Utility Aircraft
Original language description
This paper deals with aeroelastic certification analyses of the new generation Czech twin turboprop utility aircraft. Paper is focused to the first phase of analyses before the ground vibration test (GVT) of the prototype. It describes the analytical model as well as the used tools and methods. The description of specific blocks of analyses follows afterwards. It includes the preliminary flutter analyses, static aeroelastic analyses (control reversal and divergence), modal analyses and large parametricflutter analyses (surface, control surfaces and tab flutter). The flutter characteristics of the structure with respect to changes of the selected parameters are presented. Furthermore the preparation of the GVT, i.e. the optimization of the exciter andaccelerometer positions based on the analytical results, and the whirl flutter analyses by means of an optimization-based approach to find the critical stability boundaries are explained. Finally, the performed activities are summarized a
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
2011
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
Vol.225
Issue of the periodical within the volume
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Country of publishing house
GB - UNITED KINGDOM
Number of pages
10
Pages from-to
585-594
UT code for WoS article
000291492500009
EID of the result in the Scopus database
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