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° |