H-CRAFT PROJECT DESCRIPTION This year 2020/2021 I started a new academic stage at the University of Stuttgart where I had the opportunity to be involved in the Aircraft Design Seminar lectured by Herr Ingmar Geiß in collaboration with Airbus. Thanks to that I could work on a group project related to the next generation [...]
Wing Structural Analysis
Miquel Altadill2021-06-10T16:23:44+00:00WING STRUCTURAL ANALYSIS PROJECT DESCRIPTION As it is well known an aircraft wing structure purpose is to keep the wing skin fixed at the same time that it holds the weight of the engines and the fuel tanks in some cases. The mean idea is to develop an inner lightweight structure capable of holding [...]
Northern Ice
Miquel Altadill2021-06-10T16:23:52+00:00NORTHERN ICE CONCENTRATION PROJECT DESCRIPTION These recent days I read a question that got stuck into my mind, what would you be now if you got your childhood dreamed job? What an easy question, isn’t it? What I had and I still have clear is that I wanted to be an engineer that worked [...]
Airfoil Design
Miquel Altadill2021-06-10T16:24:02+00:00AIRFOIL DESIGN PROJECT DESCRIPTION The main objective of this project is to propose a suitable airfoil for a reliable commercial aircraft based on Hydrogen propulsion systems. My Airfoil Design was a project developed in the IAG department of the University of Stuttgart for the Airfoil Design Seminar. Working together with the help of Dr. [...]
Potential FLow
Miquel Altadill2021-06-10T16:24:07+00:00POTENTIAL FLOW PROJECT DESCRIPTION This project was developed in the Computational Engineering subject taken during my MSc in Aeronautic Engineering at the UPC – ESEIAAT. It was developed under the supervision of the Dr. Carlos David Perez Segarra in the CTTC department. The project consisted on the application of the Potential Flow theory for [...]
Convection Diffusion
Miquel Altadill2021-06-10T16:24:12+00:00CONVECTION – DIFFUSION PROJECT DESCRIPTION This project was developed in the Computational Engineering subject taken during my MSc in Aeronautic Engineering at the UPC – ESEIAAT. It was developed under the supervision of the Dr. Carlos David Perez Segarra in the CTTC department.. The numerical solution of heat transfer, fluid flow, and other related [...]





