In this paper we carry out a linear stability analysis within the Stok
es layer that, under suitable conditions, forms at the surface of a ci
rcular cylinder in periodic orbital motion. The analysis is related to
that performed by Seminara [1, 2] in the Stokes layer on a torsionall
y oscillating cylinder and by Hall [3] in the Stokes layer at the surf
ace of a cylinder in purely oscillatory motion. In ail cases we find t
hat the minimum critical Taylor number is located where the flow at th
e edge of the Stokes layer has maximum speed in each period of the mot
ion.