Simulation tool to predict the aerodynamics of tilt-wing aircraft - Texte

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Forschungsstelle

INNOSUISSE

Projektnummer

106.064.1 IP-ENG

Projekttitel

Simulation tool to predict the aerodynamics of tilt-wing aircraft

Projekttitel Englisch

Simulation tool to predict the aerodynamics of tilt-wing aircraft

Texte zu diesem Projekt

	Deutsch	Französisch	Italienisch	Englisch
Kurzbeschreibung		-	-
Abstract		-	-

Erfasste Texte

Kategorie	Text
Kurzbeschreibung (Deutsch)	Simulation tool to predict the aerodynamics of tilt-wing aircraft
Kurzbeschreibung (Englisch)	Simulation tool to predict the aerodynamics of tilt-wing aircraft
Abstract (Deutsch)	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.
Abstract (Englisch)	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.