Project number
25059
Organization
UA Department of Aerospace and Mechanical Engineering
Offering
ENGR498-F2024-S2025
This project introduces a versatile UAV testbed designed to support on-demand analysis of various flight configurations with a single aircraft with the goal of enhancing flight research capabilities at U of A.
The team developed the UAV testbed through extensive research into construction techniques and aircraft performance to ensure the design aligns with conventional aerodynamics while maintaining modular adaptability. The resulting airframe prioritizes ease of assembly and positive stability across a wide range of configurations. To optimize performance, the team estimated the flight envelope using numerical analysis and simulations and ensured structural integrity before fabrication using finite element analysis.
A hands-on manufacturing approach played a key role in development. Prior material testing helped determine the optimal fabrication methods for carbon fiber composites, which were primarily produced in-house. Pre-manufactured carbon tubes and outsourced machined aluminum parts complemented the custom-built components. This resulted in a lightweight yet structurally robust aircraft.
The UAV features a speed range of 45 to 200 mph, a wing sweep angle adjustable from 0 to 60 degrees, and a 10 ft wingspan at 45 degrees sweep. With a flight time of five to seven minutes, it meets all research requirements set by U of A and provides a highly adaptable platform for advanced aerodynamic testing.
The team developed the UAV testbed through extensive research into construction techniques and aircraft performance to ensure the design aligns with conventional aerodynamics while maintaining modular adaptability. The resulting airframe prioritizes ease of assembly and positive stability across a wide range of configurations. To optimize performance, the team estimated the flight envelope using numerical analysis and simulations and ensured structural integrity before fabrication using finite element analysis.
A hands-on manufacturing approach played a key role in development. Prior material testing helped determine the optimal fabrication methods for carbon fiber composites, which were primarily produced in-house. Pre-manufactured carbon tubes and outsourced machined aluminum parts complemented the custom-built components. This resulted in a lightweight yet structurally robust aircraft.
The UAV features a speed range of 45 to 200 mph, a wing sweep angle adjustable from 0 to 60 degrees, and a 10 ft wingspan at 45 degrees sweep. With a flight time of five to seven minutes, it meets all research requirements set by U of A and provides a highly adaptable platform for advanced aerodynamic testing.