Aerodynamic measurements on airfoils in the wind tunnel

This research project is to better understand the flight dynamic characteristics of airfoils. The candidate will conduct an experimental study of the flow around airfoils in the wind tunnel. He will analyze the data to characterize the spatio-temporal dynamics of the vortex structures produced. The experimental study will be conducted in the wind tunnel located at the Université de Sherbrooke (UdeS). It has a closed test section of 1.82m×1.82m, and a maximum speed of 35 m/s. Some of these equipment’s will be used: Particle Image Velocimetry (PIV) and Hot Wire Anemometry (HWA).

Faculty Supervisor:

Hachimi Fellouah

Student:

SARAHI ANGUIANO GUTIERREZ

Partner:

Discipline:

Engineering - mechanical

Sector:

University:

Program:

Globalink

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