Blow-down wind tunnel

Test section : 0.6m×1.2m×2.4m

6 components force balance with 2D positionning system for pitch and yaw

Flow speed up to U=30m/s with 1% turbulent intensity

Stereoscopic PIV system 100Hz, pressure scanners, hot wires anemometry


Aerodynamics and drag reduction of an Ahmed body at variable attitude

Drone aerodynamics and wake Interactions

Bluff body aerodynamics in inhomogeneous and unsteady incoming flows

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