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
Projects
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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