Wayfarer

In the early Phase I stages, my responsibility encompassed modeling the C182 baseline aircraft. Specifically, I focused on digitizing the geometry of our physical test bed. This involved creating a low-fidelity model that featured a relatively high-fidelity wing. The purpose of this modeling was to facilitate the design of essential hardware components needed for the seamless installation of the planned modifications. 

In addition to my prior tasks, I was entrusted with the responsibility of designing and sizing the components required for a single-wing test stand. The rationale behind this initiative was to minimize both the risk and cost associated with testing before advancing to the flight test phase. Furthermore, conducting wing-only tests simplifies the data acquisition and post-processing by using a stationary DAQ system and reducing noise in the data. During this phase, I also took on miscellaneous duties, such as gathering OEM propeller geometry data encompassing chord and twist. Additionally, I played a pivotal role in preparing for Phase II, specifically in evaluating the feasibility of incorporating 3D-printed parts into the sub-scale flight test vehicle, aligning with the overarching goal of optimizing our testing procedures.