C.I.L. van der Weijst
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1 records found
1
Bachelor thesis
(2026)
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A.J.E. Brouns, E. Ceylan, C.I.L. van der Weijst, U. Dinç, W. Grefkowicz, I.S. Ivanov, L.I.F. Jordans, A. Pequeño Rodríguez, D. Roos, B.D. Taskin, B.E.G. Verhoef, F. Scarano, R.P. Dwight, N. Dhiman, S.J. Randeraad
Vold-e is a fully electric autonomous eVTOL designed for urban and regional air mobility. Its key innovation is a folding Prandtl wing, which reduces ground footprint while maintaining aerodynamic efficiency. The aircraft carries four passengers, has a range of 200 km, and reaches speeds of 200 km/h.
The design combines six electric rotors, a lightweight composite structure, and advanced autonomous control systems with redundant safety features. Aerodynamic and structural analyses confirm that the aircraft is feasible, with strong efficiency and stability performance. Vold-e also offers zero in-flight CO₂ emissions, reduced land use, and competitive future operating costs. The main challenges are technical complexity, certification, and market adoption. ...
The design combines six electric rotors, a lightweight composite structure, and advanced autonomous control systems with redundant safety features. Aerodynamic and structural analyses confirm that the aircraft is feasible, with strong efficiency and stability performance. Vold-e also offers zero in-flight CO₂ emissions, reduced land use, and competitive future operating costs. The main challenges are technical complexity, certification, and market adoption. ...
Vold-e is a fully electric autonomous eVTOL designed for urban and regional air mobility. Its key innovation is a folding Prandtl wing, which reduces ground footprint while maintaining aerodynamic efficiency. The aircraft carries four passengers, has a range of 200 km, and reaches speeds of 200 km/h.
The design combines six electric rotors, a lightweight composite structure, and advanced autonomous control systems with redundant safety features. Aerodynamic and structural analyses confirm that the aircraft is feasible, with strong efficiency and stability performance. Vold-e also offers zero in-flight CO₂ emissions, reduced land use, and competitive future operating costs. The main challenges are technical complexity, certification, and market adoption.
The design combines six electric rotors, a lightweight composite structure, and advanced autonomous control systems with redundant safety features. Aerodynamic and structural analyses confirm that the aircraft is feasible, with strong efficiency and stability performance. Vold-e also offers zero in-flight CO₂ emissions, reduced land use, and competitive future operating costs. The main challenges are technical complexity, certification, and market adoption.