A Numerical Approach for Wind Tunnel Noise Control

Detta är en Master-uppsats från KTH/Marcus Wallenberg Laboratoriet MWL

Sammanfattning: A wind tunnel from the 1950s located in Bromma, Stockholm, once used for military research is today used for commercial activities. Today the tunnel is used for indoor wingsuit flight and the facility has an interest in reducing the overall noise generated by the tunnel. Acoustic measurements indicate noise problems in the 50 Hz range. A 3D and a 2D model was structured with physical measured dimensions of the wind tunnel for simulations.Results indicate that a 37 dB decrease of the second higher order azimuthal spinning mode was achievable with the same number of monopole anti-sources as fan blades with each individual monopole modeling an enclosed loudspeakers. This acoustic mode was identified as the most problematic due to the cut-on frequency for the geometry coinciding with the fundamental blade pass frequency of the fan source during normal operating conditions.

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