The basic aerodynamic characteristics of twin cable were investigated throu
gh a series of wind tunnel tests employing full aeroelastic twin cable mode
l. The cable arrangement employed here is characterized by W/D ratio that v
aries from 4.3 to 8.7 (where W is the spacing of centers of cables, D is th
e diameter of the cable), namely corresponds to the value between the criti
cal condition of 'wake-galloping' and the so-called 'wake induced flutter'.
Consequently, in the case where W/D equals 4.3, though typical wake-gallop
ing vibration was observed, relatively small additional damping was effecti
ve to mitigate the vibration. In the cases where W/D is larger than 6.5, th
e model was found to be stable. Moreover, dominant vibratory axis of the le
eward cable was found to be dependent on both Reynolds number and reduced w
ind speed, through the investigation changing the natural frequency of the
cable model. (C) 2000 Elsevier Science Ltd. All rights reserved.