Mathematical Problems in Engineering / 2017 / Article / Fig 10

Research Article

Wind Tunnel Tests on Aerodynamic Characteristics of Ice-Coated 4-Bundled Conductors

Figure 10

Effect of bundle space on the aerodynamic characteristics of subconductor 2 (thickness: 10 (30) mm, initial ice accretion angle: 0°).
(a)  mm, initial ice accretion angle = 0°
(b)  mm, initial ice accretion angle = 0°
(c)  mm, initial ice accretion angle = 0°
(d)  mm, initial ice accretion angle = 0°

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