1. Create, grade assignments/projects, and host office hours.2. Teach MATLAB, SolidWorks, ethics, and engineering design.

1. Developing a left ventricle mock circulation loop to simulate and test cardiac pumps.2. Using data acquisition techniques to obtain pressure, flow data, and PIV (Particle Image Velocimetry).3. Employing data analysis techniques to study flow structure inside the left ventricle.

1. Create, grade assignments/projects, and host office hours.2. Help students understand key concepts like propeller selection and design, lifting line theory, powerplant matching, blade momentum theory, vortex lattice methods, propeller performance curves, actuator disk theory, and cavitation.

Designing, building, and testing an acoustic enclosure for high power steady-state lasers, prone to acoustic interference when in the presence of high amplitude and low-frequency noise sources.

Aided in imaging module redesign research. The project is motivated by separate NAVAIR and Pratt and Whitney funded research efforts studying cutting edge multi-property measurements of vector velocity, temperature, and density in varying flow environments using Filtered Rayleigh scattering (FRS). My primary responsibility on this project was to provide a detailed design of a new imaging module for FRS measurements using Solidworks.

Nalu Medical, Inc. is an upcoming company in neurostimulation technology. As an intern my roles were:1. Design and create assemblies/parts via Solidworks.2. Prepare documentation for design, testing and validation of class II medical devices per FDA standards in an ISO 13485 regulated environment.3. Execute test protocols to validate designs for 510K submissions.4. Prepare standard operating procedure (SOP) for the upcoming projects.

A member of low level controls sub-team. Used Raspberry Pi and Arduino interconnected with Robotic Operating Software (ROS) to tackle the agBOT 2019 challenge.

Performed finite element analysis (ANSYS) on the rocket bulkheads. The analysis also helped optimize the bulkhead design eliminating non-load bearing material, hence making it cheaper as well as reducing the dry mass of the rocket.