Portfolio showing the extra-curricular skills and tools learnt throughout a Sheffield aerospace engineering MEng degree: specialising in CAD (Siemens NX and Fusion), CFD (Ansys Fluent/ Meshing), FEA (Ansys Mechanical), Control Theory (Simulink) and Data analysis (MATLAB/ Python). These projects begin with a goal and navigate through engineering processes to a validated result.
65% Mass Reduction · +0.14 Safety Margin
Mach 2.0 · 24° Ramp · Shock-Induced Separation
2000 - 5500 rpm · 2.54 N Thrust Per Propeller
Fully Parameterised · 6000 rpm · 3000K Spark
61° Phase Margin · ~10% Overshoot · All Poles LHP