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The uSeeding LDV system provises a additional tool to explore this challengeeginn.
However, our well-established Boundary Layer Wind Tunnels produce straight and steady wind and are limited in Reynolds number.
Modeling of these features is underscored by the difficulty in matching supercritical Reynolds number in boundary layer wind tunnels.
Results have been compared to the available experimental data from previous studies in boundary layer wind tunnels.
Roughness elements are usually added in boundary layer wind tunnels to enhance the energy of certain turbulence scales and their range.
Many types of meteorological, environmental and boundary layer wind tunnels have been constructed to simulate atmospheric phenomena on buildings and structures.
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The experiments were conducted in a boundary layer wind tunnel.
Simulation results are compared to wind tunnel experiments conducted in a boundary layer wind tunnel.
The wind tunnel experiments are performed in an atmospheric boundary layer wind tunnel at scale 1 100.
Boundary layer wind tunnel testing using pressure-tap models is effective for measuring these pressures.
Boundary layer wind tunnel tests were performed on a model of a cantilever grandstand.
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