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Unité de recherche
INNOSUISSE
Numéro de projet
106.064.1 IP-ENG
Titre du projet
Simulation tool to predict the aerodynamics of tilt-wing aircraft
Titre du projet anglais
Simulation tool to predict the aerodynamics of tilt-wing aircraft

Textes relatifs à ce projet

 AllemandFrançaisItalienAnglais
Description succincte
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Résumé des résultats (Abstract)
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Textes saisis


CatégorieTexte
Description succincte
(Allemand)
Simulation tool to predict the aerodynamics of tilt-wing aircraft
Description succincte
(Anglais)
Simulation tool to predict the aerodynamics of tilt-wing aircraft
Résumé des résultats (Abstract)
(Allemand)
Dufour is designing electrical vertical take-off and landing aircraft. They teamed up with the Centre for Aviation at ZHAW to develop a numerical tool for aerodynamic predictions on the behavior of their aircraft. Wind tunnel tests will be carried out to ensure the accuracy of the developed tool.
Résumé des résultats (Abstract)
(Anglais)
Dufour is designing electrical vertical take-off and landing aircraft. They teamed up with the Centre for Aviation at ZHAW to develop a numerical tool for aerodynamic predictions on the behavior of their aircraft. Wind tunnel tests will be carried out to ensure the accuracy of the developed tool.