Goh Qi Xuan

- Characterized a hypersonic wind tunnel (Ludwieg Tube) for scientific use by validating operational envelope - Conducted over 120 wind tunnel test campaigns, gaining deep understanding of concept of converging-diverging nozzle - Data analysis of high-speed aerothermodynamic measurement (shockwave, heat flux, pitot pressure) relevant to UAV and reentry vehicles

- Designed and manufactured a custom high-precision pressure sensor rake tailored to wind tunnel characteristic. - Calibrated sensors, integrated electronics, and selected measurement instruments along with respective Software. - Organized the Bill of Materials (BOM) for test models, ensuring manufacturability, quality compliance, and procurement efficiency - Documented test reports and the safety user manual of wind tunnel with 20MPa and 900K storage tank capacity

- Integrated, calibrated sensors and executed pressure, wind velocity measurement in Göttingen-style low-speed wind tunnel - Optimized costs in boundary layer investigations by redesigning sensor materials and built components

Core Subjects: Aerodynamics, Numerical Fluid Dynamics, Flight Propulsion, Aerospace Materials, Thermodynamics