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LATEST PROJECTS

The purpose of this research was to determine the aerodynamic efficiency, stability and loads carried by the structure of 3 different models of wings for Pterosaurs in gliding condition.
 
During this placement AVL, X-Foil and XFLR5 software were used for the aerodynamic analyses and Matlab code for the structural analyses. The research concluded with the selection of the most appropriate approximation of wing model, and therefore, the most likely to have belonged to the winged reptile.
​An investigation aimed to design an UAV and a class K solid motor rocket capable to impulse the aircraft from 200 km/h to 700 km/h in less than five (5) seconds. It included the construction and testing of the aircraft. 

Position: Propulsion system designer (Rocket motor)

If you require any additional information please do not hesitate to contacting me >>>

Aerodynamic and Structural

Analysis of the flight of

a Pteranodon

Thermal modelling and assessment

of high temperature materials and technologies for use in a 100W water resistojet

Design of an Unnamed Aerial Vehicle 

-UAV- powered with a rocket motor

The purpose of this research was to develop a thermal modelling analysis, using ANSYS Workbench, of emerging concepts for electrical propulsion application into small satellites. It included the construction and testing of a optomised prototype which was able to increase the specific impulse in 20% in reference to the original.
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