The third wind tunnel section is suitable for basic and applied research applications. It can be used for testing 2D aifoils, aircraft wings, fuselages, model aircrafts, light and heavy vechicles. It is equipped with a high accuracy six-component balance for the measurement of the airloads.
Testing of an aircraft in the 1.8x1.4m section
Wing model for testing 2D airfoils
Flow visualization around a 1/18 scale car model
Aerodynamic coefficients, velocity and pressure around a 1/5 scale model
Aerodynamic study of an electric vehicle designed in the laboratory
Research of the aerodynamic coefficients, static stability characteristics and the tank trajectory after release from an airplane model
