L inf. -Optimal Feed-forward Gust Load Alleviation Design for a large Blended Wing Body Airliner
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F11%3A00181538" target="_blank" >RIV/68407700:21230/11:00181538 - 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
L inf. -Optimal Feed-forward Gust Load Alleviation Design for a large Blended Wing Body Airliner
Original language description
The potential advantages of Blended Wing Body (BWB) aircraft in terms of fuel efficiency are opposed by technical challenges such as the alleviation of gust loads. Due to the low wing loading gusts generally have a more severe impact on BWB aircraft thanon conventional aircraft. This paper presents the design and optimisation of a Gust Load Alleviation System (GLAS) for a large BWB airliner. Numeric simulations are performed with an aeroelastic model of the aircraft including GLAS in order to compute time series of modal displacements for deriving equivalent static load cases which are used for resizing of the aircraft structure.
Czech name
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Czech description
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Classification
Type
O - Miscellaneous
CEP classification
BC - Theory and management systems
OECD FORD branch
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Result continuities
Project
<a href="/en/project/7E08041" target="_blank" >7E08041: Active Control for Flexible 2020 Aircraft</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2011
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů