The aerodynamic instability of a long-span suspension bridge with a shallow
streamlined box girder is a serious engineering concern, particularly duri
ng the early deck erection stage. Its characteristics are significantly inf
luenced by the sequence of deck erection. Using the Hoga Kusten Bridge in S
weden as an example, this paper presents an analytical and experimental dis
cussion regarding the evolution of flutter characteristics for a long-span
suspension bridge, and a comparison of different erection sequences and ana
lytical prediction of more stable configurations. The general feature of th
e flutter limit evolution with the erection program of midspan to pylons, w
hich was previously evidenced by wind tunnel tests, has been successfully r
eproduced analytically, and the advantages of keeping nonsymmetric deck con
figurations were confirmed. The pylon to midspan program has never been emp
loyed for long-span girder bridges, but it was found to be, at least, aerod
ynamically favorable.