Gust Load Alleviation on 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%3A21220%2F10%3A00179195" target="_blank" >RIV/68407700:21220/10:00179195 - 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
Gust Load Alleviation on a Large Blended Wing Body Airliner
Original language description
This paper investigates the gust load response of a large 750 passenger Blended Wing Body (BWB) airliner for identification of sizing cases for the aircraft structure. Considering manoeuvre load alleviation, gust loads become the dominant sizing factor for the BWB airplane. In order to allow for structural weight saving a Gust Load Alleviation System (GLAS) is designed and evaluated by numeric simulations.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
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Continuities
R - Projekt Ramcoveho programu EK
Others
Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
ICAS 2010 27th Congress
ISBN
978-0-9565333-0-2
ISSN
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e-ISSN
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Number of pages
10
Pages from-to
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Publisher name
Optimage
Place of publication
Edinburgh
Event location
Nice
Event date
Sep 19, 2010
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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