2019
DOI: 10.1016/j.buildenv.2019.04.013
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Effect of local and upwind stratification on flow and dispersion inside and above a bi-dimensional street canyon

Abstract: The effects of a stably-stratified boundary layer on flow and dispersion in a bi-dimensional street canyon with unity aspect ratio have been investigated experimentally in a wind tunnel in combination with differential wall heating. Laser-Doppler anemometry together with a fast flame ionisation detector and cold-wire anemometry were employed to sample velocities, concentration, temperatures and fluxes.A single-vortex pattern was observed in the isothermal case, preserved also when leeward wall was heated, but … Show more

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Cited by 41 publications
(16 citation statements)
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References 36 publications
(65 reference statements)
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“…Each measurement point was sampled for 2.5 minutes, following previous experiments in neutral (Castro et al, 2017) and non-neutral (Marucci and Carpentieri, 2019a) conditions. The standard errors for first and second order statistics was evaluated at each measurement point and deemed satisfactory for high-quality experiments (see, in particular, Marucci and Carpentieri, 2019b).…”
Section: Experimental Methodologymentioning
confidence: 99%
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“…Each measurement point was sampled for 2.5 minutes, following previous experiments in neutral (Castro et al, 2017) and non-neutral (Marucci and Carpentieri, 2019a) conditions. The standard errors for first and second order statistics was evaluated at each measurement point and deemed satisfactory for high-quality experiments (see, in particular, Marucci and Carpentieri, 2019b).…”
Section: Experimental Methodologymentioning
confidence: 99%
“…Surface aerodynamic (friction velocity u * , roughness length z 0 , displacement height d, BL detpth δ) and thermal (scaling temperature θ * = − w θ 0 /u * , thermal roughness length z 0h , thermal displacement height d h ) were estimated as described in details by Marucci and Carpentieri (2019a) and Marucci and Carpentieri (2019b), by fitting the logarithmic profiles and the vertical shear stress profiles. Other values reported in the table are a reference temperature close to the floor (Θ 0 ), the temperature at the boundary-layer height (Θ δ ), a velocity scale valid on the mixed layer of a CBL, defined as (Kaimal and Finnigan, 1994):…”
Section: Approaching Flow and Boundary Layer Over The Arraymentioning
confidence: 99%
“…The measurement setup was identical to the one used by Marucci and Carpentieri (2019b), to which we refer the reader for more details. Temperatures and two components of velocity were measured simultaneously using, respectively, a fast-response cold-wire probe (CW) and a laser Doppler anemometer (LDA).…”
Section: Measurementsmentioning
confidence: 99%
“…The LDA target acquisition frequency was set to 100 Hz, while temperatures were sampled at 1000 Hz. Given the irregular nature of the LDA measurements and the different frequencies, a resampling and synchronisation of the three signals was necessary for computing heat fluxes (Marucci and Carpentieri, 2019b). The measurement rig also included a fast flame ionisation detector (FFID) to measure tracer concentrations, even though concentration and mass flux results are not reported here (see, e.g.…”
Section: Measurementsmentioning
confidence: 99%
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