Investigation of the Aerodynamic Characteristics of Platoon Vehicles Based on Ahmed Body

Figure 15

x-direction velocity contour and streamline distribution behind trailing body in three bodies on xz symmetry plane. (a) x/L = 0.25 (b) x/L = 0.5. (c) x/L = 0.75. (d) x/L = 1. (e) x/L = 1.25. (f) x/L = 1.5.

(a)

(b)

(c)

(d)

(e)

(f)