A snapshot of my ongoing work across multidisciplinary aircraft design optimization and propulsion lab experimentation.
My current work centers on developing an MDO algorithm for rapid electric aircraft conceptual design. This framework was also used by the Purdue SAE Aero Design Team during the competition aircraft conceptual design stage to compare configurations and make faster design decisions.
The objective is to connect sizing, performance, and mission-level constraints in one modular workflow so early design iterations remain rigorous while still moving quickly.
Submitted abstract documenting the MDO framework and conceptual design application.
At Prof. Nicole Key's High Speed Compressor Lab (Fall 2025 onward), I contributed to inlet vortex distortion studies and experimental hardware readiness, including fan-rig assembly and calibration support.