Asymptotic theory of high-aspect-ratio wings in steady incompressible
flow is extended to a case where the wing forms either an open or clos
ed circular are. The generalization is based on an integral formulatio
n of the problem, which resembles the one used by Guermond (1990) for
a plane curved wing. A second-order approximation is obtained for the
load distribution on two model wings, one resembling that of a gliding
parachute, and the other resembling a short duct.