We expand the variables as
and in this article neglect terms of order
O(
δ2) and higher. Where necessary in the following, we denote by
U,
V, and
W the components of
U in the directions of increasing
r,
ϑ, and
φ, respectively, and we use the subscripts 0 and 1 to denote their contributions to
U0 and
U1, respectively.
At
O(
δ0), the problem is in the spherical geometry
r ≤ 1, and it was solved by David et al.
19 We briefly recap the solution: The continuity equation (11
b) and the
r- and
ϑ-components of equation (11
a) decouple from the
φ-component of (11
a), and thus since the right-hand side of the boundary condition (12) is purely in the
φ-direction, only the
φ-component of the velocity is nonzero. The solution is
where
a =
αce−iπ/4. Substituting into equations (9) and (13) gives the leading-order contribution to the stress as
At
O(
δ1) we use the fact that any smooth scalar function can be written as a sum of scalar spherical harmonics,
Ymn, and a vector-valued function as a sum of vector spherical harmonics,
Pmn,
Bmn, and
Cmn. The reader is referred to other literature
23 for a detailed definition of the vectors
Pmn,
Bmn, and
Cmn, but here we remark that for a particular
m and
n they are pairwise orthogonal, with
Pmn always in the radial direction and
Bmn and
Cmn spanning the zenithal and azimuthal directions. We expand the velocity and pressure as
where
U1mn(
r),
V1mn(
r),
W1mn(
r), and
(
r) are functions to be found.
The boundary conditions are projected onto
r =
1, a description of which appears in the literature,
21 and become
so that
V̂mn and
Ŵmn depend on the choice of shape through
R 1.
Substituting into the governing equations (11
a,b) we obtain a system of ordinary differential equations that can be solved to obtain
for n > 0, and
=
= 0, where
Jk denotes the Bessel function of order
k,
sn =
, and the boundary condition (18) implies
The stress at order
δ can be calculated from the formula