Development of a low-order aerodynamic performance model tailored for large aspect ratio wings with distributed hybrid-electric propulsion
25 March 2024
๐ Exciting News from the INDIGO Team! ๐
26 August 2024
Airframe mass estimation methods for large aspect ratio wings
Moving forward!
The INDIGO research team at the Aeroelastic and Structural Design Lab at the UC3M Aerospace Engineering department is developing airframe mass estimation methods for large aspect ratio wings with distributed hybrid-electric propulsion based on structural optimisation as part of the INDIGO project Task 1.4. Special thanks to Joรฃo Carvalho and Antonio Raimondo for their valuable contributions to the research activity.
Our photo gallery regarding this great development below!
