Hypersonic Ramjet/Scramjet RL Control
Built a Reinforcement Learning controlled ramjet/scramjet engine simulation with DARE and CVODE for reacting-flow ODEs. Modeled fuel-flow control via equivalence ratio across Mach 1–5 and 1k–50k ft.
Built a Reinforcement Learning controlled ramjet/scramjet engine simulation with DARE and CVODE for reacting-flow ODEs. Modeled fuel-flow control via equivalence ratio across Mach 1–5 and 1k–50k ft.
Coordinated cross-functional development of a biodegradable water pellet for autonomous aerial firefighting. Defined test methodology and maintained full DFMEA and engineering requirements.
CHARM Lab — Researched and prototyped novel pneumatic actuators for medical soft robotics. Programmed Arduino-based active pressure regulation, modeled dynamics in MATLAB, and prototyped with ultrasonic welding.
Boeing Test & Evaluation — Designed and executed thermal/pressure tests for T-7A advanced trainer aircraft inlet ducts. Developed and automated LabVIEW DAQ systems for flight hardware qualification.
FX Lab — Designed a precision HSI test platform with PID feedback control. Integrated thermocouple and RTD sensors for precise thermal profiles. 3D-printed custom nozzle geometries for uniform velocity fields.
Boeing — Designed and 3D-printed airflow plenums for Low Earth Orbit satellite heat transfer experiments. Modeled convective heat transfer in orbital thermal environments.
Designed and built a hierarchical multi-agent system using large language models, where a central orchestrator delegates tasks to specialized sub-agents. Agents coordinate through structured tool calls, memory, and message passing to solve complex multi-step engineering problems.