SAE Aero Design Challenge
Problem
Statement
Develop an aircraft capable of carrying maximum payload with minimum weight possible
52732702_430227301051202_7686763079849976870_n.mp4Competition flight
Development
Led a team of students in development of high payload capacity aircraft for SAE Aero Design Challenge 2018.
Modelled and analyzed aircraft using Solidworks, devised onboard mechanisms, and manufactured prototypes using 3D printing, Laser cutting, and aluminum welding to keep weight and cost of aircraft as minimum as possible.
Developed a Rectangular Taper wing design that resulted in 250% load-lift capacity with minimal turbulence and achieved assembly in <20 seconds using design protocol based on Design for Assembly principles.
Strategized aircraft design, encompassing assembly approach, quick payload release mechanisms, and flight plan and secured 10th place in debut year.
Team
I managed this small and interdisciplinary team, it was challenging, but I was able to orchestrate the team's workflow processes effectively. By distributing tasks and assignments across the team, we were able to achieve optimal progress while minimizing delays and ensuring everyone's involvement in the project's success.
Overall, this project was a fantastic example of what can be achieved when a team of diverse individuals comes together to pursue a common goal. I'm incredibly proud of what we accomplished, and I believe this experience has taught us all valuable lessons about teamwork, perseverance, and the power of creativity and collaboration.
Designed, manufactured and iterated aircraft
Skills : Solidworks, CNC machining, 3D printing, Lathe, manufacturing, controls
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