OA-004 / Project
Aug 2025 – Present
Design/Build/Fly Aircraft Work
Cut airframe drag 18% and body weight 34% through geometry optimization and carbon-fiber fabrication.
As Aerodynamics / Manufacturing Engineer for Gator Design/Build/Fly, I model lifting-surface aerodynamics in ANSYS Fluent and XFLR5 to predict stall behavior and size control surfaces, and manufacture carbon fiber airframe structure. Iterative geometry optimization and composite fabrication reduced airframe drag by 18% and body weight by 34%.
Role
Aerodynamics / Manufacturing Engineer
Organization
University of Florida · Gator Design/Build/Fly
Manufacturing the airframe
I manufacture airframe structure for Gator Design/Build/Fly, including the carbon fiber fuselage, using positive carbon fiber molding to lay up parts.
Through iterative geometry optimization and carbon-fiber composite fabrication, we reduced airframe drag by 18% and body weight by 34%, while keeping layup quality, part fit, and structure strong enough to survive a competition airframe.
Aerodynamics in ANSYS Fluent and XFLR5
I model lifting-surface aerodynamics in ANSYS Fluent and XFLR5 to predict stall behavior and optimize control-surface sizing. On Prototype 1, a standard layout with one nose wheel and two rear wheels, I checked lift, induced and viscous drag, surface velocity, pressure, and downwash to understand how the airframe would behave before flight.
Interactive 3D CAD
Drag to rotate, scroll to zoom.