Knowledge Based Engineering framework for preliminary spaceplane design

The concept of a spaceplane, a launch system that is a combination of an airplane and a rocket, is one of the most promising concepts of sustainable access to space. Along its trajectory, it experiences most extreme conditions with frequently opposing design requirements, making it one of the most complicated challenges in aerospace engineering....

Simulation & Analysis of the Aerodynamic Interactions between Distributed Propellers and Wings

The recent advances in complementary technologies have given a new impulse in the research activities related to distributed propulsion. Light electric engines, whose performance is rather insensitive to scaling, improved battery capacities and autonomous flight all contribute to this trend. Promising concepts featuring electrically powered...

A numerical investigation into the aerodynamic characteristics of AeroCity

An Investigation of the Non-Linear 3D Flow Effects Relevant for Leading Edge Inflatable Kites

The kite power group at TU Delft is currently researching the use of leading edge inflatable (LEI) kites for use in power generation. A thorough understanding of the aeroelastics of these kites is paramount to the development of system simulation models and optimum kite and system designs. The current lack of understanding is therefore seen as a...