Multidisciplinary design optimization (MDO) is a technique that has found use in the field of aerospace engineering for aircraft design. It uses optimization to simultaneously solve design problems with several disciplines involved. In order to predict aircraft performance an engine Continue reading
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Tag: Space
Value stream mapping for an office environment (Mechanical/Aeronautical Project)
To be more flexible and efficient in a process, lean and all of its methods can be used to improve your workplace. This study was carried out by two aeronautical engineering students from Continue reading
Injector design and test for a high power electrodeless plasma thruster (Mechanical Project)
The HPEP (High Performance Electric Propulsion) thruster is expected to be the outcome of an innovative project initiated by the Swedish Space Corporation. It combines the concept of a 10 kW electrodeless plasma thruster designed by the Elwing Company and the Continue reading
Assembly of a UAV (Unmanned Aerial Vehicle): hardware design of a UAV (Electronics Project)
This project is dedicated to assemble the hardware system of a UAV (Unmanned Aerial Vehicle) in order to prepare the platform for an autonomous flight in the air for a given path through the pre-programmed check points. A UAV is an aircraft that contains Continue reading
An Explication of Airfoil Section Bending-Torsion Flutter (Civil Project)
This study examines the dynamic instability known as flutter using a two-degree-of-freedom airfoil section model in both quasi-steady and unsteady flow. It explains the fundamental forces and moments involved in the Continue reading
Analysis of Metal to Composite Adhesive Joins in Space Applications (Mechanical Project)
Within the European space program, a new upper stage engine (Vinci) for the Ariane 5 launcher is being developed, and the Volvo Aero Corporation (VAC) is contributing with Continue reading
Study of 3-Dimensional Co-Flow Jet Airplane and High-Rise Building Flow Using CFD Simulation (Mechanical Project)
The purpose of this thesis is to design and study an aircraft which implements the Co-Flow Jet (CFJ) airfoil concept, as well as to study the CAARC standard highrise building. The design concept is verified mainly by the use of a Computational Fluid Dynamics (CFD) package. A thorough methodology for Continue reading
Augmented Reality for Space Applications (Robotics Project)
Future space exploration will inevitably require astronauts to have a higher degree of autonomy in decision-making and contingency identification and resolution. Space robotics will eventually become a Continue reading