Assessment of Aileron Tab Installation Influence to Aircraft Flutter Characteristics
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F14%3A%230001690" target="_blank" >RIV/00010669:_____/14:#0001690 - isvavai.cz</a>
Result on the web
<a href="http://arc.aiaa.org/doi/abs/10.2514/6.2011-1849" target="_blank" >http://arc.aiaa.org/doi/abs/10.2514/6.2011-1849</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.2514/6.2011-1849" target="_blank" >10.2514/6.2011-1849</a>
Alternative languages
Result language
angličtina
Original language name
Assessment of Aileron Tab Installation Influence to Aircraft Flutter Characteristics
Original language description
This paper deals with the aileron flutter of the ultra-light aircraft. It gives an assessment of influence of the retrofitting of the tab regarding the aircraft aileron flutter characteristics. The necessary actuation system stiffness and the aileron flapping frequency to ensure the stability at the aircraft maximal speed are evaluated. The work was motivated by the M-7 ultra light aircraft accident in the western Bohemia in 2006. The FE model was prepared by the optimization approach. The design variables were mass and stiffness characteristics, design responses (constrains and objective functions) were given from the ground vibration tests data.
Czech name
—
Czech description
—
Classification
Type
D - Article in proceedings
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
—
Result continuities
Project
—
Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2014
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference Proceedings
ISBN
978-1-60086-951-8
ISSN
—
e-ISSN
—
Number of pages
10
Pages from-to
—
Publisher name
American Institute of Aeronautics and Astronautics (AIAA)
Place of publication
USA
Event location
Denver, CO, USA
Event date
Jan 1, 2011
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
—