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

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Research unit

INNOSUISSE

Project number

106.064.1 IP-ENG

Project title

Simulation tool to predict the aerodynamics of tilt-wing aircraft

Texts for this project

	German	French	Italian	English
Short description		-	-
Abstract		-	-

Inserted texts

Category	Text
Short description (German)	Simulation tool to predict the aerodynamics of tilt-wing aircraft
Short description (English)	Simulation tool to predict the aerodynamics of tilt-wing aircraft
Abstract (German)	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 (English)	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.