Aerodynamic Optimization and Boundary Layer Control on Sailplane Wing Sections
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F07%3A00152569" target="_blank" >RIV/68407700:21220/07:00152569 - 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
Aerodynamic Optimization and Boundary Layer Control on Sailplane Wing Sections
Original language description
Numerical analysis tools have been thoroughly verified and coupled with findings of wind-tunnel and flight evaluations. Optimization procedure has been used for multicriteria sailplane airfoil design with using of fitness function. Surface visualizationhas been carried out and separation regions along the wingspan studied on wings of two club class sailplanes. Passive flow control has been consequently applied at optimum location. Glide ratio has been measured and significant performance improvement has been gained.
Czech name
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Czech description
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Classification
Type
O - Miscellaneous
CEP classification
BK - Liquid mechanics
OECD FORD branch
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Result continuities
Project
<a href="/en/project/1M06059" target="_blank" >1M06059: Advanced Technologies and Systems for Power Engineering</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2007
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů