Research Article

Wind Tunnel Measurement of Turbulent and Advective Scalar Fluxes: A Case Study on Intersection Ventilation

Figure 7

Dimensionless velocity fields for four angles of the approach flow direction.
381357.fig.007a
(a) Approach flow 𝜑 = 0
381357.fig.007b
(b) Approach flow 𝜑 = 5
381357.fig.007c
(c) Approach flow 𝜑 = 1 5
381357.fig.007d
(d) Approach flow 𝜑 = 4 5