FLUTTER ANALYSIS OF THE AIRPLANE HARMONY
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F22%3A00370966" target="_blank" >RIV/68407700:21220/22:00370966 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
FLUTTER ANALYSIS OF THE AIRPLANE HARMONY
Original language description
Report describes experimental modal analysis of the whole airplane with evaluation of results. The process of experimental determination and evaluation of mass characteristic for lifting surfaces and control surfaces of the airplane is included in the report. In addition, the flutter analysis based on those data is carried out by p-k methods. The influence of towing device and autopilot is included in the flutter analysis.
Czech name
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Czech description
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Classification
Type
O - Miscellaneous
CEP classification
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OECD FORD branch
20304 - Aerospace engineering
Result continuities
Project
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Continuities
N - Vyzkumna aktivita podporovana z neverejnych zdroju
Others
Publication year
2022
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů