This project focuses on the design, construction, and operation of a small-scale wind tunnel environment designed to simulate real-world flight conditions. By bridging the gap between theoretical fluid dynamics and physical prototyping, this testbed serves as a critical platform for analyzing airfoil performance. Through the development of custom fixtures and the use of flow visualization techniques, the project explores the fundamental relationship between lift and the angle of attack, providing essential data on stall behavior. This hands-on experience in experimental design and instrument calibration mirrors the workflows found in high-level aerospace labs, specifically those dedicated to UAV development and CubeSat deployable systems.