Wing Geometry Design Using Glauert?s Method
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F15%3APU118753" target="_blank" >RIV/00216305:26210/15:PU118753 - isvavai.cz</a>
Alternative codes found
RIV/00216305:26210/15:PU118763
Result on the web
<a href="http://www.engmech.cz/2015/im/doc/pdf/EA_Koutnik_155.pdf" target="_blank" >http://www.engmech.cz/2015/im/doc/pdf/EA_Koutnik_155.pdf</a>
DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Wing Geometry Design Using Glauert?s Method
Original language description
Glauert's solution of Prandtl's lifting line theory is quick method widely used for analysis of spanwise lift distribution on planar wings. In this article, its use on an inverse problem is demonstrated. The concept is tested by morphing the initial rectangular wing planform to reach demanded lift distribution. Results are compared with theoretical assumptions and with solution obtained from CFD simulation.
Czech name
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Czech description
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Classification
Type
O - Miscellaneous
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
<a href="/en/project/LO1202" target="_blank" >LO1202: NETME CENTRE PLUS</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2015
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů