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1. Enabling high-fidelity measurements of turbulent boundary layer flow over wing sections in the MTL wind tunnel.
Master-uppsats, KTH/MekanikSammanfattning : A reinforced fiber-glass model of a NACA 4412 wing profile is designed and set-up in the Minimum Turbulence Level (MTL) wind tunnel facility at KTH. The model has 65 pressure taps orifices, and the set-up includes two mounting panels designed to allow for particle image velocimetry (PIV) and hot wire anemometry (HWA) measurements of the boundary layer (to be performed in a future campaign). LÄS MER
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