Mechanical Concepts for Simulation of Nonlinearities on Aeroelastic Demonstrator

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F14%3A%230001688" target="_blank" >RIV/00010669:_____/14:#0001688 - isvavai.cz</a>
Result on the web
<a href="http://arc.aiaa.org/doi/pdfplus/10.2514/1.C031760" target="_blank" >http://arc.aiaa.org/doi/pdfplus/10.2514/1.C031760</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.2514/1.C031760" target="_blank" >10.2514/1.C031760</a>

Result language
angličtina
Original language name
Mechanical Concepts for Simulation of Nonlinearities on Aeroelastic Demonstrator
Original language description
This paper deals with the mechanical concept of aeroelastic demonstrator of the aircraft wing/engine. It describes the component for simulation of non-linearities, such as nonlinear passive engine suspension stiffness and nonlinear active aileron actuation stiffness. The paper is focused on the development and testing of the nonlinear components and comparison of the test results and simulations. Demonstrator is exploited within the research projects for the research and development of the new methods of the ground vibration testing including nonlinearities.
Czech name
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Czech description
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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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Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2014
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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