Aerodynamic Optimization and Boundary Layer Control on Sailplane Wing Sections

Kód výsledku v 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>
Výsledek na webu
—
DOI - Digital Object Identifier
—

Jazyk výsledku
angličtina
Název v původním jazyce
Aerodynamic Optimization and Boundary Layer Control on Sailplane Wing Sections
Popis výsledku v původním jazyce
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.
Název v anglickém jazyce
Aerodynamic Optimization and Boundary Layer Control on Sailplane Wing Sections
Popis výsledku anglicky
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.

Projekt
<a href="/cs/project/1M06059" target="_blank" >1M06059: Progresivní technologie a systémy pro energetiku</a><br>
Návaznosti
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění
2007
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Podobné výsledky(10)