Rigid Wing CAD Design
• MSc student in the field of structures, materials and manufacturing, or other relevant fields.
• Experience with CAD.
• Experience with FEM.
• Eager to learn and good team worker.
• Proficient in English.
• Affinity with UAV’s and sustainable technology is a plus.
A conceptual design for a rigid wing airborne wind energy system with a nominal power output of 750 kW has been made, based on top-level requirements, with a focus on manufacturability, damage resistance, and maintenance. This conceptual design has to be downscaled to a system with a nominal power output of 100 kW, and elaborated into a detailed design.