The Aerodynamics Loads of the Wing-Winglet Configuration for UL and VLA Aircraft

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F08%3APU77350" target="_blank" >RIV/00216305:26210/08:PU77350 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
The Aerodynamics Loads of the Wing-Winglet Configuration for UL and VLA Aircraft
Original language description
The determination of so-called "air loads" is one of the first and basic tasks of the solving team in the process of designing aircraft. The paper describes the use of the CFD analysis results in the determination of various aerodynamic loads cases of the wing-winglet configuration for UL and VLA aircraft.
Czech name
Aerodynamické zatížení konfigurace křídlo-winglet u ultralehkých letadel
Czech description
The determination of so-called "air loads" is one of the first and basic tasks of the solving team in the process of designing aircraft. The paper describes the use of the CFD analysis results in the determination of various aerodynamic loads cases of the wing-winglet configuration for UL and VLA aircraft.

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
<a href="/en/project/1M0501" target="_blank" >1M0501: Aerospace Research Centre</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2008
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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